Infeed assembly full inspection assembly

ABSTRACT

An infeed assembly for a necker machine includes a full inspection assembly wherein the full inspection assembly is structured to be coupled to a necker machine frame assembly.

CROSS REFERENCE TO RELATED APPLICATIONS

This application claims priority to U.S. Provisional Application No.62/070,196, filed May 11, 2018, entitled, INFEED ASSEMBLY FULLINSPECTION ASSEMBLY.

BACKGROUND OF THE INVENTION Field of the Invention

The disclosed and claimed concept relates to a necking machine and, inparticular, to a necking machine with a full inspection assembly.

Background Information

The can bodies are, typically, formed in a bodymaker. That is, abodymaker forms blanks such as, but not limited to, disks or cups intoan elongated can body. A can body includes a base and a dependingsidewall. The sidewall is open at the end opposite the base. Thebodymaker, typically, includes a ram/punch that moves the blanks througha number of dies to form the can body. The can body is ejected from theram/punch for further processing such as, but not limited to, trimming,washing, printing, flanging, inspecting, and placed on pallets which areshipped to the filler. At the filler, the cans are taken off of thepallets, tilled, ends placed on them and then the filled cans arerepackaged in six packs and/or twelve pack cases, etc.

Some can bodies are further formed in a necking machine (also identifiedas a “necker” machine). Necking machines are structured to reduce thecross-sectional area of a portion of a can body sidewall, i.e., at theopen end of the sidewalk That is, prior to coupling a can end to the canbody, the diameter/radius of the can body sidewall open end is reducedrelative to the diameter/radius of other portions of the can bodysidewall. The necking machine includes a number of processing and/orforming stations disposed in series. That is, the processing and/orforming stations are disposed adjacent to each other and a transferassembly moves a can body between adjacent processing and/or formingstations. As the can body moves through the processing and/or formingstations it is processed or formed. A greater number of processingand/or forming stations in a necking machine is not desirable. That is,it is desirable to have the least number of processing and/or formingstations possible while still completing the desired forming.

Further, it is desirable to have the least number of processing and/orforming stations possible so as to occupy the least amount of floorspace. Some of this floor space is occupied by an infeed assembly and anumber of inspection devices. That is, the inspection devices areincorporated into the infeed assembly. Typically, some printingoperations are performed prior to necking operations. Thus, a can bodyabout to be necked could have any number of defects such as, but notlimited to defects in the shape of the can body (typically caused byforming operations such as in the bodymaker) and/or defects in theprinting on the can body. The can bodies are inspected prior to formingoperations in the necking machine. That is, inspection devices perform anumber of inspections and, if a can body is found to be defective, thecan body is ejected from the necking machine,

One problem with known necking machine inspection devices is that theinspection devices do not, perform the full range of inspections, towhich a can body is, or should be, subjected. Notably, known inspectionsystems fail to perform inspections for label (printing) verificationand sidewall damage. Further, the inspection devices must be disposedalong the work path of the can bodies. That is, as used herein, to bepart of the necking machine the, inspection devices must be mounted onthe necking machine. If an inspection device is not mounted on thenecking machine, it is, as used herein, an “external inspection device.”

It is generally acknowledged, however, that a necking machine does nothave sufficient space to accommodate a number of different types ofinspection devices that are desired. That is, most inspection devicesare disposed at the upstream end of the work path of the can bodies andat or near, an infeed assembly. The work path of the can bodies at, ornear, an infeed assembly is generally closed (the can bodies are notgenerally accessible for inspection) and/or is occupied by otherequipment. Thus, the inspection devices cannot be disposed along thework path of the can bodies at the infeed assembly. That is, in theknown art, only a few inspection devices are, and can be, disposed alongthe work path of tile can bodies at the infeed assembly because there isinsufficient space adjacent the open portions (wherein the can bodiesare generally accessible for inspection). This is a problem. That is, ifthe inspection devices are disposed downstream of the infeed assembly,forming operations will be performed on (possibly) deformed can bodies.

Further, it is not desirable to extend the length of the work path ofthe can bodies at the infeed assembly. That is, as noted above, it isdesirable to have the least number of processing and/or forming stationspossible so as to occupy the least amount of floor space. Adding lengthto the necking machine so as to accommodate additional inspectiondevices simply adds to the length of the necking machine and is not adesirable solution. That is, the length of the necking machine is aproblem when the necking machine is longer, i.e., occupies more space,than is needed. Thus, the lack of a full inspection assembly is aproblem.

Further, some known inspection devices are not disposed at the upstreamend of the necking machine. That is, some inspection devices aredisposed at the downstream end of the necking machine even though theinspection device checks for defects that exist in the can body prior tonecking operations. These are problems because performing neckingoperations on a defective can body is a waste of time. That is, thedefective can body will, eventually, be identified and the can bodyremoved from further processing. Thus, any effort to neck a defectivecan body is wasted. Thus, the lack of an upstream inspection assembly isa problem.

Further, can bodies with defective shapes may not operate effectivelywith the necking machine. That is, defects in the shape of the can bodymay cause the can body to be ejected prematurely, and/or in anuncontrolled manner, from the necking machine. This is also a problembecause an uncontrolled ejection of a can body may damage components ofthe necking machine and/or the inspection devices. Further, performingnecking operations on defective can bodies reduce the efficiency of thenecking machine. That is, even if a defective can body is necked, thecan body is not usable; thus, the number of useable can bodies producedby the necking machine over a period of time is reduced. Thus,processing defective can bodies is a problem.

There is, therefore, a need for an infeed assembly that inspects canbodies upstream of other processing stations. There is a further needfor an infeed assembly that ejects defective can bodies prior to theother processing stations.

SUMMARY OF THE INVENTION

These needs, and others, are met by at least one embodiment of thedisclosed and claimed concept which includes an infeed assembly for anecker machine, the necker machine including a frame assembly, thenecker machine frame assembly having an upstream end and a downstreamend, the necker machine defining a work path having an upstream end anda downstream end. The infeed assembly includes a full inspectionassembly wherein the full inspection assembly is structured to becoupled to the necker machine frame assembly. The infeed assembly alsoincludes an ejection assembly. Thus, the infeed assembly solves theproblems stated above.

BRIEF DESCRIPTION OF THE DRAWINGS

A full understanding of the invention can be gained, from the followingdescription of the preferred embodiments when read in conjunction withthe accompanying drawings in which:

FIG. 1 is an isometric view of a necker machine.

FIG. 2 is another isometric view of a necker machine.

FIG. 3 is a front view of a necker machine.

FIG. 4 is a schematic cross-sectional view of a can body.

FIG. 5 is an isometric view of an infeed assembly.

FIG. 6 is a partial isometric view of an infeed assembly,

FIG. 7 is another partial isometric view of an infeed assembly.

FIG. 8 is another partial isometric view of an infeed assembly.

FIG. 9 is partial cross-sectional view of an infeed assembly.

FIG. 10 is another partial isometric view of an infeed assembly.

FIG. 11 is an isometric view of a quick-change vacuum starwheelassembly.

FIG. 12 is a partial cross-sectional view of a quick-change vacuumstarwheel assembly.

FIG. 13 is a detail, partial cross-sectional view of a travelerassembly.

FIG. 14 is a front view of a quick-change vacuum starwheel assembly.

FIG. 15 is an isometric view of a vacuum assembly telescoping vacuumconduit.

FIG. 16 is a cross-sectional side view of a vacuum assembly telescopingvacuum conduit.

FIG. 17 is a back view of a vacuum assembly.

FIG. 18 is a side view of a vacuum assembly.

FIG. 19 is an isometric view of a vacuum assembly.

FIG. 20A is an isometic view of a quick-change height adjustmentassembly traveling hub assembly. FIG. 20B is cross-sectional side viewof a quick-change height adjustment assembly traveling hub assembly.FIG. 20C is a front view of a quick-change height adjustment assemblytraveling hub assembly.

FIG. 21 is an isometric view of a traveling hub assembly positioning keyassembly.

FIG. 22 is a partial cross-sectional side view of a traveling hubassembly positioning key assembly.

FIG. 23 is a detail cross-sectional side view of a traveling hubassembly positioning key assembly.

FIG. 24 is an end view of a traveling hub assembly positioning keyassembly.

FIG. 25 is an isometric view of one traveling hub assembly positioningkey assembly wedge body.

FIG. 26 is an isometric view of the other traveling hub assemblypositioning key assembly wedge body.

FIG. 27 is an isometric view of a forming station.

FIG. 28 is an isometric view of an outboard turret assembly positioningkey.

FIG. 29 is an isometric view of an outboard turret assembly pusher ramblock positioning key mounting.

FIG. 30 is an isometric view of a pusher assembly.

FIG. 31 is another isometric view of a pusher assembly.

FIG. 32 is a cross-sectional view of a pusher assembly.

FIG. 33 is an isometric cross-sectional view of a portion of a pusherassembly.

FIG. 34 is a detail cross-sectional view of a pusher assembly.

FIGS. 35A-35E are isometric views of an outer die assembly quick-changedie assembly with the elements in different configurations.

FIG. 36 is an end view of an outer die assembly quick-change dieassembly.

FIG. 37A is an isometric, exploded view of another embodiment of anouter die assembly quick-change die assembly. FIG. 37B is an isometricview of an outer die assembly quick-change coupling.

FIGS. 38A-38C are isometric views of another embodiment of an outer dieassembly quick-change die assembly with the elements in differentconfigurations.

FIG. 39 is an isometric cross-sectional view of the embodiment of anouter die assembly quick-change die assembly shown in FIG. 38C.

FIG. 40 is an isometric view of a portion of an inner die assemblyquick-change die assembly.

FIG. 41 is another isometric view of a portion of an inner die assemblyquick-change die assembly.

FIG. 42 is a detail isometric view of a portion of an inner die assemblyquick-change die assembly.

FIG. 43 is a cross-sectional view of an inner die assembly quick-changedie assembly.

FIG. 44 is an isometric view of another embodiment of an outer dieassembly quick-change die assembly.

FIG. 45 is a detail isometric view of the embodiment of an outer dieassembly quick-change die assembly shown in FIG. 44.

FIG. 46 is an axial view of a rotary manifold.

FIG. 47 is a radial cross-sectional view of a rotary manifold.

FIG. 48 is an axial cross-sectional view of a rotary manifold.

FIG. 49 is a rear view of a drive assembly.

FIG. 50 is a rear view of selected elements of a drive assembly.

FIG. 51 is a cross-sectional view of drive assembly components.

FIG. 52 is an isometric view of drive assembly components.

FIG. 53 is an isometric view of other drive assembly components.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

It will be appreciated that the specific elements illustrated in thefigures herein and described in the following specification are simplyexemplary embodiments of the disclosed concept, which are provided asnon-limiting examples solely for the purpose of illustration. Therefore,specific dimensions, orientations, assembly, number of components used,embodiment configurations and other physical characteristics related tothe embodiments disclosed herein are not to be considered limiting onthe scope of the disclosed concept.

Directional phrases used herein, such as, for example, clockwise,counterclockwise, left, right, top, bottom, upwards, downwards andderivatives thereof, relate to the orientation of the elements shown inthe drawings and are not limiting upon the claims unless expresslyrecited therein.

As used herein, the singular form of “a,” and “the” include pluralreferences unless the context clearly dictates otherwise.

As used herein, “structured to [verb]” means that the identified elementor assembly has a structure that is shaped, sized, disposed, coupledand/or configured to perform the identified verb. For example, a memberthat is “structured to move” is movably coupled to another element andincludes elements that cause the member to move or the member isotherwise configured to move in response to other elements orassemblies. As such, as used herein, “structured to [verb]” recitesstructure and not function. Further, as used herein, “structured to[verb]” means that the identified element or assembly is intended to,and is designed to, perform the identified verb. Thus, an element thatis merely capable of performing the identified verb but which is notintended to, and is not designed to, perform the identified verb is not“structured to [verb].”

As used herein, “associated” means that the elements are part of thesame assembly and/or operate together, or, act upon/with each other insome manner. For example, an automobile has four tires and four hubcaps. While all the elements are coupled as part of the automobile, itis understood that each hubcap is “associated” with a specific tire.

As used herein, a “coupling assembly” includes two or more couplings orcoupling components. The components of a coupling or coupling assemblyare generally not part of the same element or other component. As such,the components of a “coupling assembly” may not be described at the sametime in the following description.

As used herein, a “coupling” or “coupling component(s)” is one or morecomponent(s) of a coupling assembly. That is, a coupling assemblyincludes at least two components that are structured to be coupledtogether. It is understood that the components of a coupling assemblyare compatible with each other. For example, in a coupling assembly, ifone coupling component is a snap socket, the other coupling component isa snap plug, or, if one coupling component is a bolt, then the othercoupling component is a nut or threaded bore. Further, a passage in anelement is part of the “coupling” or “coupling component(s).” Forexample, in an assembly of two wooden boards coupled together by a nutand a bolt extending through passages in both boards, the nut, the boltand the two passages are each a “coupling” or “coupling component.”

As used herein, a “fastener” is a separate component structured tocouple two or more elements. Thus, for example, a bolt is a “fastener”but a tongue-and-groove coupling is not a “fastener,” That is, thetongue-and-groove elements are part of the elements being coupled andare not a separate component.

As used herein, a “retained” coupling means a coupling component(s) thatwhile movable, cannot be separated from an associated element. Forexample, on an automobile, a lug nut tethered to a wheel is a “retained”coupling. That is, in use, the lug nut extends through a wheel hub andis coupled to an axle hub thereby coupling the wheel to the axle. Whenthe wheels need to be rotated, the lug nut is decoupled from an axle hubthereby decoupling the wheel from the axle hub. The tethered lug nutcannot, however, be decoupled from the wheel hub due to the tether. Inthis configuration, the lug nut cannot be misplaced. Any of the retainedcouplings described below are alternately a “release coupling,” a“retained release” coupling or a “reduced actuation” coupling. Use of a“retained” coupling solves the problems discussed above.

As used herein, a “release” coupling is two or more coupling componentsthat move between a secure/tight position and a loose position relativeto each other. During normal use, the elements of a “release” couplingare not separated. For example, a hose clamp including an elongated,slotted, looped body and a threaded fastener rotatably mounted thereonis a “release” coupling. As is known, utilizing the threaded fastener todraw the looped body in one direction tightens the hose clamp about ahose while extending the looped body loosens the hose clamp. Duringnormal use, the looped body and the fastener are not separated. Any ofthe release couplings described below are alternately a “retained”coupling, a “retained release” coupling or a “reduced actuation”coupling. Use of a “release” coupling solves the problems discussedabove.

As used herein, a “retained release” coupling is a release couplingwherein the elements of the release coupling are not separable from theelement(s) to which the release couplings are coupled. For example, ahose clamp that is tethered to the hose which it clamps is a “retainedrelease” coupling. Any of the retained release couplings described beloware alternately a “retained” coupling, a “release” coupling or a“reduced actuation” coupling. Use of a “retained release” couplingsolves the problems discussed above.

As used herein, a “reduced actuation” coupling means a coupling thatmoves between a secure/locked/engaged position and areleased/unlocked/disengaged position with a minimal action. As usedherein, a “minimal action” means less than a 360° rotation for rotatingcouplings. Any of the reduced actuation couplings described below arealternately a “retained” coupling, a “release” coupling or a “retainedrelease” coupling. Use of a “reduced actuation” coupling solves theproblems discussed above.

As used herein, the statement that two or more parts or components are“coupled” shall mean that the parts are joined or operate togethereither directly or indirectly, i.e., through one or more intermediateparts or components, so long as a link occurs. As used herein, “directlycoupled” means that two elements are directly in contact with eachother. As used herein, “fixedly coupled” or “fixed” means that twocomponents are coupled so as to move as one while maintaining a constantorientation relative to each other. As used herein, “adjustably fixed”means that two components are coupled so as to move as one whilemaintaining a constant general orientation or position relative to eachother while being able to move in a limited range or about a singleaxis. For example, a doorknob is “adjustably fixed” to a door in thatthe doorknob is rotatable, but generally the doorknob remains in asingle position relative to the door. Further, a cartridge (nib and inkreservoir) in a retractable pen is “adjustably fixed” relative to thehousing in that the cartridge moves between a retracted and extendedposition, but generally maintains its orientation relative to thehousing. Accordingly, when two elements are coupled, all portions ofthose elements are coupled. A description, however, of a specificportion of a first element being coupled to a second element, e.g., anaxle first end being coupled to a first wheel, means that the specificportion of the first element is disposed closer to the second elementthan the other portions thereof. Further, an object resting on anotherobject held in place only by gravity is not “coupled” to the lowerobject unless the upper object is otherwise maintained substantially inplace. That is, for example, a book on a table is not coupled thereto,but a book glued to a table is coupled thereto.

As used herein, the phrase “removably coupled” or “temporarily coupled”means that one component is, coupled with another component in anessentially temporary manner. That is, the two components are coupled insuch a way that the joining or separation of the components is easy andwould not damage the components. For example, two components secured toeach other with a limited number of readily accessible fasteners, i.e.,fasteners that are not difficult to access, are “removably coupled”whereas two components that are welded together or joined by difficultto access fasteners are not “removably coupled.” A “difficult to accessfastener” is one that requires the removal of one or more othercomponents prior to accessing the fastener wherein the “other component”is not an access device such as, but not limited to, a door.

As used herein, “operatively coupled” means that a number of elements orassemblies, each of which is movable between a first position and asecond position, or a first configuration and a second configuration,are coupled so that as the first element moves from oneposition/configuration to the other, the second element moves betweenpositions/configurations as well. It is noted that a first element maybe “operatively coupled” to another without the opposite being true.

As used herein, “temporarily disposed” means that a first element(s) orassembly (ies) is resting on a second element(s) or assembly(ies) in amanner that allows the first element/assembly to be moved without havingto decouple or otherwise manipulate the first element. For example, abook simply resting on a table, i.e., the book is not glued or fastenedto the table, is “temporarily disposed” on the table.

As used herein, the statement that two or more parts or components“engage” one another means that the elements exert a force or biasagainst one another either directly or through one or more intermediateelements or components. Further, as used herein with regard to movingparts, a moving part may “engage” another element during the motion fromone position to another and/or may “engage” another element once in thedescribed position. Thus, it is understood that the statements, “whenelement A moves to element A first position, element A engages elementB,” and “when element A is in element A first position, element Aengages element B” are equivalent statements and mean that element Aeither engages element B while moving to element A first position and/orelement A either engages element B while in element A first position.

As used herein, “operatively engage” means “engage and move.” That is,“operatively engage” when used in relation to a first component that isstructured to move a movable or rotatable second component means thatthe first component applies a force sufficient to cause the secondcomponent to move. For example, a screwdriver may be placed into contactwith a screw. When no force is applied to the screwdriver, thescrewdriver is merely “temporarily coupled” to the screw. If an axialforce is applied to the screwdriver, the screwdriver is pressed againstthe screw and “engages” the screw. However, when a rotational force isapplied to the screwdriver, the screwdriver “operatively engages” thescrew and causes the screw to rotate. Further, with electroniccomponents, “operatively engage” means that one component controlsanother component by a control signal or current.

As used herein, “correspond” indicates that two structural componentsare sized and shaped to be similar to each other and may be coupled witha minimum amount of friction. Thus, an opening which “corresponds” to amember is sized slightly larger than the member so that the member maypass through the opening with a minimum amount of friction. Thisdefinition is modified if the two components are to fit “snugly”together. In that situation, the difference between the size of thecomponents is even smaller whereby the amount of friction increases. Ifthe element defining the opening and/or the component inserted into theopening are made from a deformable or compressible material, the openingmay even be slightly smaller than the component being inserted into theopening. With regard to surfaces, shapes, and lines, two, or more,“corresponding” surfaces, shapes, or lines have generally the same size,shape, and contours.

As used herein, a “path of travel” or “path,” when used in associationwith an element that moves, includes the space an element moves throughwhen in motion. As such, any element that moves inherently has a “pathof travel” or “path.” Further, a “path of travel” or “path” relates to amotion of one identifiable construct as a whole relative to anotherobject. For example, assuming, a perfectly smooth road, a rotating,wheel (an identifiable construct) on an automobile generally does notmove relative to the body (another object) of the automobile. That is,the wheel, as a whole, does not change its position relative to, forexample, the adjacent fender. Thus, a rotating wheel does not have a“path of travel” or “path” relative to the body of the automobile.Conversely, the air inlet valve on that wheel (an identifiableconstruct) does have a “path of travel” or “path” relative to the bodyof the automobile. That is, while the wheel rotates and is in motion,the air inlet valve, as a whole, moves relative to the body of theautomobile.

As used herein, the word “unitary” means a component that is created asa single piece or unit. That is, a component that includes pieces thatare created separately and then coupled together as a unit is not a“unitary” component or body.

As used herein, the term “number” shall mean one or an integer greaterthan one (i.e., a plurality). That is, for example, the phrase “a numberof elements” means one element or a plurality of elements. It isspecifically noted that the term “a ‘number’ of [X]” includes a single[X].

As used herein, a “limited number” of couplings means six or fewercouplings.

As used herein, a “significantly limited number” of couplings means fouror fewer couplings.

As used herein, a “very limited number” of couplings means two or fewercouplings.

As used herein, an “exceedingly limited number” of couplings means onecoupling.

As used herein, in the phrase “[x] moves between its first position andsecond position,” or, “[y] is structured to move [x] between its firstposition and second position,” “[x]” is the name of an element orassembly. Further, when [x] is an element or assembly that moves betweena number of positions, the pronoun “its” means “[x],” i.e., the namedelement or assembly that precedes the pronoun “its”.

As used herein, a “radial side/surface” for a circular or cylindricalbody is a side/surface that extends about, or encircles, the centerthereof or a height line passing through the center thereof. As usedherein, an “axial side/surface” for a circular or cylindrical body is aside that extends in a plane extending generally perpendicular to aheight line passing through the center of the cylinder. That is,generally, for a cylindrical soup can, the “radial side/surface” is thegenerally circular sidewall and the “axial side(s)/surface(s)” are thetop and bottom of the soup can. Further, as used herein, “radiallyextending” means extending in a radial direction or along a radial line.That is, for example, a “radially extending” line extends from thecenter of the circle or cylinder toward the radial side/surface.Further, as used herein, “axially extending” means extending in theaxial direction or along an axial line. That is, for example, an“axially extending” line extends from the bottom of a cylinder towardthe top of the cylinder and substantially parallel to a centrallongitudinal axis of the cylinder.

As used herein, “generally curvilinear” includes elements havingmultiple curved portions, combinations of curved portions and planarportions, and a plurality of planar portions or segments disposed atangles relative to each other thereby forming a curve.

As used herein, a “planar body” or “planar member” is a generally thinelement including opposed, wide, generally parallel surfaces, i.e., theplanar surfaces of the planar member, as well as a thinner edge surfaceextending between the wide parallel surfaces. That is, as used herein,it is inherent that a “planar” element has two opposed planar surfaces.The perimeter, and therefore the edge surface, may include generallystraight portions, e.g., as on a rectangular planar member, or becurved, as on a disk, or have any other shape.

As used herein, for any adjacent ranges that share a limit, e.g., 0%-5%and 5%-10, or, 0.05 inch-0.10 inch and 0.001 inch-0.05 inch, the upperlimit of the lower range, i.e., 5% and 0.05 inch in the examples above,means slightly less than the identified limit. That is, in the exampleabove, the range 0%-5% means 0%-4.999999% and the range 0.001 inch-0.05inch means 0.001 inch-0.04999999 inch.

As used herein, “upwardly depending” means an element that extendsupwardly and generally perpendicular from another element.

As employed herein, the terms “can” and “container” are usedsubstantially interchangeably to refer to any known or suitablecontainer, which is structured to contain a substance (e.g., withoutlimitation, liquid; food; any other suitable substance), and expresslyincludes, but is not limited to, beverage cans, such as beer andbeverage cans, as well as food cans.

As used herein, a “product side” means the side of a container thatcontacts, or could contact, a product such as, but not limited to, afood or beverage. That is, the “product side” of the construct is the eof the construct that, eventually, defines the interior of a container.

As used herein, a “customer side” means the side of a construct used ina container that does not contact, or could not contact, a product suchas, but not limited to, a food or beverage. That is, the “customer side”of the construct is the side of the construct that, eventually, definesthe exterior of a container.

As used herein, “about” in a phrase such as “disposed about [an element,point or axis]” “extend about [an element, point or axis]” or “[X]degrees about an [an element, point or axis],” means encircle, extendaround, or measured around. When used in reference to a measurement orin a similar manner, “about” means “approximately,” i.e., in anapproximate range relevant, to the measurement as would be understood byone of ordinary skill in the art.

As used herein, a “drive assembly” means elements that are operativelycoupled to the rotating shafts extending back to front in a processingstation. A “drive assembly” does not include the rotating shaftsextending back to front in a processing station.

As used herein, a “lubrication system” means a system that applies alubricant to the external surfaces of a linkage, e.g., shafts and gears,of a drive assembly.

As used herein, an “elongated” element inherently includes alongitudinal axis and/or longitudinal line extending in the direction ofthe elongation.

As used herein, “generally” means “in a general manner” relevant to theterm being modified as would be understood by one of ordinary skill inthe art.

As used herein, “substantially” means “for the most part” relevant tothe term being modified as would be understood by one of ordinary skillin the art.

As used herein, “at” means on and/or near relevant to the term beingmodified as would be understood by one of ordinary skill in the art.

As shown in FIGS. 1-3, a necker machine 10 is structured to reduce thediameter of a portion of a can body 1. As used herein, to “neck” meansto reduce the diameter/radius of a portion of a can body 1. That, is, asshown in FIG. 4, a can body 1 includes a base 2 with an upwardlydepending sidewall 3. The can body base 2 and can body sidewall 3 definea generally enclosed space 4. In the embodiment discussed below, the canbody 1 is a generally circular and/or an elongated cylinder. It isunderstood that this is only one exemplary shape and that the can body 1can have other shapes. The can body has a longitudinal axis 5. The canbody sidewall 3 has a first end 6 and, a second end 7. The can body base2 is at the second end 7. The can body first end 6 is open. The can bodyfirst end 6 initially has substantially the same radius/diameter as thecan body sidewall 3. Following forming operations in the necker machine10, the radius/diameter of the can body first end 6 is smaller than theother portions of the radius/diameter at the can body sidewall 3.

The necker machine 10 includes an infeed assembly 100, a plurality ofprocessing/forming stations 20, a transfer assembly 30, and a driveassembly 2000 (FIG. 49). Hereinafter, processing/forming stations 20 areidentified by the term “processing stations 20” and refer to genericprocessing stations 20. Specific processing stations, which are includedin the collective group of “processing stations 20,” are discussed belowand are given a separate reference number. Each processing station 20has a width which is generally the same as all other processing stations20. Thus, the length/space occupied by the necker machine 10 isdetermined by the number of processing stations 20.

As is known, the processing stations 20 are disposed adjacent to eachother and in series. That is, the can bodies 1 being processed by thenecker machine 10 each move from an upstream location through a seriesof processing stations 20 in the same sequence. The can bodies 1 followa path, hereinafter, the “work path 9.” That is, the necker machine 10defines the work path 9 wherein can bodies 1 move from an ‘upstream’location to a “downstream” location; as used herein, “upstream generallymeans closer to the infeed assembly 100 and “downstream” means closer toan exit assembly 102. With regard to elements that define the work path9, each of those elements have an “upstream” end and a “downstream end”wherein the can bodies move from the upstream” end to the “downstreamend.” Thus, as used herein, the nature/identification of an elementassembly, sub-assembly, etc. as an “upstream” or “downstream” element orassembly, or, being in an “upstream” or “downstream” location, isinherent. Further, as used herein, the nature/identification of anelement, assembly, sub-assembly, etc. as an “upstream” or “downstream”element or assembly, or, being in an “upstream” or “downstream”location, is a relative term.

As noted above, each processing station 20 has a similar width and thecan body 1 is processed and/or formed (or partially formed) as the canbody 1 moves across the width. Generally, the processing/forming occursin/at a turret 22. That is, the term “turret 22” identifies a genericturret. As discussed below, each processing station 20 includes anon-vacuum starwheel 24. As, used herein, a “non-vacuum starwheel” meansa starwheel that does not include, or is not associated with, a vacuumassembly 480, discussed below, that is structured to apply a vacuum tothe starwheel pockets 34, discussed below. Further, each processingstation 20 typically includes one turret 22 and one non-vacuum starwheel24.

The transfer assembly 30 is structured to move the can bodies 1 betweenadjacent processing stations 20. The transfer assembly 30 includes aplurality of vacuum starwheels 32. As used herein, a “vacuum starwheel”means a starwheel assembly that includes, or is associated with, avacuum assembly 480 that is structured to apply a vacuum to thestarwheel pockets 34. Further, the term “vacuum starwheel 32” identifiesa generic vacuum starwheel 32. Specific vacuum starwheels, e.g., “fullinspection assembly first vacuum starwheel 220,” are discussed below inassociation with specific processing stations 20. As discussed in detailbellow, a vacuum starwheel 32 includes disk-like, body (or disk-likebody assembly such as the vacuum starwheel body assembly 450, discussedbelow and shown in FIG. 11) and a plurality of pockets 34 disposed onthe radial surface of the disk like body. When used in association withgenerally cylindrical can bodies 1, the pockets 34 are generallysemi-cylindrical. A vacuum assembly 480, discussed below, selectivelyapplies suction to the pockets 34 and is structured to selectivelycouple a can body 1 to a pocket 34. It is understood, and as usedherein, that “to apply a vacuum to a pocket 34” means that a vacuum (orsuction) is applied to a starwheel pocket radially extending passage470, discussed below. As such, components of the transfer assembly 30such as, but not limited to, the vacuum starwheels 32 are alsoidentified as parts of the processing stations 20. Conversely, thenon-vacuum starwheel 24 of the processing stations 20 also move the canbodies 1 between processing stations 20 so the non-vacuum starwheels 24are also identified as part of the transfer assembly 30. Each of thesestarwheel assemblies 24, 32 are discussed below.

It is, however, noted that the plurality of processing stations 20 arestructured to neck different types of can bodies 1 and/or to neck canbodies in different configurations. Thus, the plurality of processingstations 20 are structured to be added and removed from the neckermachine 10 depending, upon the need. To accomplish this, the neckermachine 10 includes a frame assembly 12 to which the plurality ofprocessing stations 20 are removably coupled. Alternatively, the frameassembly 12 includes elements incorporated into each of the plurality ofprocessing station 20 so that the plurality of processing stations 20are structured to be temporarily coupled to each other. The frameassembly 12 has an upstream end 14 and a downstream end 16. Further, theframe assembly 12 includes elongated members, panel members (neithernumbered), or a combination of both. As is known, panel members coupledto each other, or coupled to elongated members, form a housing.Accordingly, as used herein, a housing is also identified as a “frameassembly 12.”

The infeed assembly 100 is structured to feed individual can bodies 1into the transfer assembly 30 which moves each can body 1 from the mostupstream processing station 20 to the most downstream processing station20, in an exemplary embodiment, the infeed assembly 100 is a “highcapacity” infeed assembly 100. As used herein, a “high capacity” infeedassembly 100 means an infeed assembly structured to feed at least 4500,and in an exemplary embodiment 4800, can bodies 1 per minute to thetransfer assembly 30.

As shown in FIG. 5, in an exemplary embodiment, the infeed assembly 100includes a “full inspection assembly” 200. As used herein, a “fullinspection assembly” 200 means an inspection assembly that is structuredto perform inspections for label verification, un-printed can, sidewalldamage, cut edge damage, bodymaker identification detection and spraydot detection. That is, the “full inspection assembly” 200 includes anumber of inspection devices 210 including a label verification assembly201 that is structured to, and does, inspect and verify that each labelis properly applied to, or printed on, each can body 1, an un-printedcan inspection assembly 202 that is structured to, and does,detect/identify can bodies 1 that have not had a label applied thereto,or printed thereon, a sidewall damage inspection assembly 203 that isstructured to, and does, inspect each can body 1 and identify can bodies1 with damaged sidewalls, a cut edge damage inspection assembly 204 thatis structured to, and does, inspect each can body 1 and identify canbodies 1 with a damaged cut edge, a bodymaker identification detectionassembly 205 that is structured to, and does, inspect each can body 1for an indicia disposed on each can body 1 by the bodymaker of the canbody 1, and a spray dot detection assembly 206 that is structured to,and does, inspect each can body 1 for an indicia disposed on each canbody 1 by lacquer applicator. These components of the full inspection,assembly 200 are collectively identified as “inspection devices” 210. Asused herein, the “inspection device(s)” 210 means any (or all) of theinspection assemblies identified above as part of a full inspectionassembly 200. Further, a full discussion of each inspection device isnot required because those systems are known in the art. It isunderstood that an inspection device 210 is, structured to, and does,inspect a can body, or portion thereof, with sensors, cameras, orsimilar devices. It is further understood that an inspection device 210is structured to, and does, produce a signal or other record indicatingthat a can body 1 is either acceptable or unacceptable.

Further, to be a “full inspection assembly” 200, as used herein, allinspection devices 210 are disposed over a limited portion of the workpath 9. As used herein, a “limited portion of the work path” means thatthe work path 9 along which the full inspection assembly 200 is disposedand structured to extend over no more than two adjacent vacuumstarwheels 32. That is, all inspection devices 210 are disposed at nomore than two adjacent vacuum starwheels 32. Further, as used herein, a“complete inspection assembly” (not shown) includes the inspectiondevices 210 of a full inspection assembly 200 as well as an ultraviolet(UV) coating inspection assembly 207 that is structured to, and does,inspect a UV coating on a can body 1. Use of a full inspection assembly200 solves the problems stated above.

Further, in an exemplary embodiment, the full inspection assembly 200 isdisposed at an upstream location relative to all processing stations 20.As used herein, an inspection assembly wherein all inspection devices ofa full inspection assembly 200 are disposed upstream relative to allprocessing stations 20 is an “upstream inspection assembly.” In thisconfiguration, the full inspection assembly 200 detects any defects inthe can bodies 1 before any forming operations occur in the neckermachine. This solves the problem(s) stated above.

That is, the infeed assembly 100 is structured to provide sufficientmounting space adjacent the work path 9 for the number of inspectiondevices 210. The full inspection assembly 100 includes a mountingassembly 212 which is structured to, and does, support the inspectiondevices. That is, the mounting assembly 212 is structured to, and does,couple, directly couple, or fix each inspection device 210 to the neckermachine frame assembly 12. In an exemplary embodiment, the fullinspection assembly mounting assembly 212 is structured to, and does,couple each inspection device 210 to the necker machine frame assembly12. Stated alternately, the full inspection assembly mounting assembly212 is structured to, and does, provide sufficient mounting space forenough inspection devices 210 to establish a full inspection assembly200. In an exemplary embodiment, the mounting assembly 212 includes anumber of guides 214. As used herein, a “mounting assembly guide” 214 isstructured to, and does, guide a can body 1 over a path so that the canbody does not contact an inspection device 210. That is, each mountingassembly guide 214 is structured to, and does, maintain a moving canbody 1 away, i.e., away from, an inspection device 210. In the priorart, there was insufficient space to accommodate a mounting assemblyguide 214 for each inspection device 210 of a full inspection assembly200. Each mounting assembly guide 214 is disposed adjacent to aninspection device 210.

That is, as noted above, the prior art does not provide sufficientmounting space in the infeed assembly 100 for enough inspection devices210 (and/or guides to protect each inspection device 210) to establish afull inspection assembly 200. The disclosed and claimed conceptaccomplishes this, in part, by providing an “effective distance” betweenadjacent vacuum starwheels 32 in the infeed assembly 100. That is, theinfeed assembly 100 includes a number of vacuum starwheels 32. To bepart of a full inspection assembly 200, as defined above, the number ofvacuum starwheels 32 is limited to two. That is, the full inspectionassembly 200 includes a first vacuum starwheel 220 and a second vacuumstarwheel 222. The full inspection assembly first vacuum starwheel 220is disposed an “effective distance” from the full inspection assemblysecond vacuum starwheel 222. As used herein, an “effective distance”means a distance that is structured to, and does, provide sufficientspace adjacent the work path 9 so as to accommodate all the inspectiondevices 210 of a full inspection assembly 200 and a mounting assemblyguide 214, and provides access to 360 degrees about a can body 1 as thecan body 1 moves over the work path 9.

As noted above, the full inspection assembly 200 includes a sidewalldamage inspection assembly 203 that is structured to, and does, inspecteach can body 1 and identify can bodies 1 with damaged sidewalls, a cutedge damage inspection assembly 204 that is structured to, and does,inspect each can body 1 and identify can bodies 1 with a damaged cutedge. It is noted that, in an exemplary embodiment, each of the sidewalldamage inspection assembly 203 and the cut edge damage inspectionassembly 204 include a camera 203′, 204′, respectively. The sidewalldamage inspection assembly camera 203′ is structured to, and does, focuson the can body sidewall 3. The cut edge damage inspection assemblycamera 204′ is structured to, and does, focus on the can body first end6. In the prior art, there was not sufficient space to mount two suchcameras on the same mounting and adjacent the work path 9. The disclosedand claimed concept provides a dual-camera mount 216 as part of themounting assembly 212. The sidewall damage inspection assembly camera203′ and the cut edge damage inspection assembly camera 204′ are eachcoupled, directly coupled, or fixed to the mounting assembly dual-cameramount 216.

The mounting assembly dual-camera mount 216 is positioned adjacent thework path 9 and is structured to, and does, position the sidewall damageinspection assembly camera 203′ to focus on the can body sidewall 3,and, position the cut edge damage inspection assembly camera 204′ tofocus on the can body first end 6. That is, as is known, a camera has afocal length. Generally, prior infeed assemblies did not have sufficientspace to allow a cut edge damage inspection assembly camera 204′disposed on the same mounting as a sidewall damage inspection assemblycamera 203′ because the cut edge damage inspection assembly camera 204′has a greater focal length compared to the sidewall damage inspectionassembly camera 203′. Because the first vacuum starwheel 220 is disposedan “effective distance” from the full inspection assembly second vacuumstarwheel 222, there is sufficient space for the dual-camera mount 216to be disposed adjacent the work path 9 with sufficient space for thecut edge damage inspection assembly camera 204′ focal length. As usedherein, such a focal length is a “cut edge damage inspection assemblycamera focal length” and means that the cut edge damage inspectionassembly camera 204′ is spaced so as to allow the cut edge damageinspection assembly camera 204′ to focus on the can body first end 6.Stated alternately, the cut edge damage inspection assembly camera 204′is coupled to the dual-camera mount 216 with sufficient spacing betweenthe cut edge damage inspection assembly camera 204′ and the work path 9to provide a cut edge damage inspection assembly camera focal length.

Further, in an exemplary embodiment, both the sidewall damage inspectionassembly camera 203′ and the cut edge damage inspection assembly camera204′ are each dual-purpose cameras. As used herein, a “dual-purposecamera” means a camera that is structured to, and does, focus, or isable to focus, on more than a single location on a work piece that isbeing inspected. When both the sidewall damage inspection assemblycamera 203′ and the cut edge damage inspection assembly camera 204′ aredual-purpose cameras, each camera 203′, 204′ is further structured toinspect additional areas of the can body 1. In an exemplary embodiment,the sidewall damage inspection assembly camera 203′ is structured to,and does, focus on both the can body sidewall 3 and the can body firstend 6. Stated alternately, the sidewall damage inspection assemblycamera 203′ is structured to, and does, inspect both the can bodysidewall 3 and the can body first end 6. Similarly, the cut edge damageinspection assembly camera 204′ is structured to, and does, focus onboth the can body sidewall 3 and the can body first end 6. Statedalternately, the cut edge damage inspection assembly camera 204′ isstructured to, and does, inspect both the can body sidewall 3 and thecan body first end 6.

Also, as noted above, the full inspection assembly 200 includes a labelverification assembly 201 that is structured to, and does, inspect andverify that each label is properly applied to, or printed on, each canbody 1, an un-printed can inspection assembly 202 that is structured to,and does, detect/identify can bodies 1 that have not had a label appliedthereto. In an exemplary embodiment, label verification assembly 201 andan un-printed can inspection assembly 202 are structured to detect colorvariation which is used to detect mixed label or unprinted can bodies 1.The mounting assembly 212 includes a “360° mounting” 218 which, as usedherein, means a mounting structured to provide a number of inspectiondevices 210 access to 360° about the can body longitudinal axis 5 and/orthe can body sidewall 3. It is understood that each of the labelverification assembly 201 and the un-printed can inspection assembly 202includes a plurality of sensors/cameras 201′, 202′. The mountingassembly 360° mounting 218 is structured to, and does, position thelabel verification assembly sensors/cameras 201′ and the un-printed caninspection assembly sensors/cameras 202′ adjacent the work path 9 sothat the plurality of label verification assembly sensors/cameras 201′and the un-printed can inspection assembly sensors/cameras 202′ have anunobstructed view of 360° about the can body longitudinal axis 5 and/orthe can, body sidewall 3. Because the first vacuum starwheel 220 isdisposed an “effective distance” from the full inspection assemblysecond vacuum starwheel 222, there is sufficient space for the mountingassembly 360° mounting 218 to be disposed adjacent the work path 9. Thelabel verification assembly sensors/cameras 201′ and the un-printed caninspection assembly sensors/cameras 202° are coupled, directly coupled,or fixed to the mounting assembly 360° mounting 218. In thisconfiguration, label verification assembly 201 and the un-printed caninspection assembly 202 (or the label verification assemblysensors/cameras 201′ and the un-printed can inspection assemblysensors/cameras 202′) are structured to, and do, inspect 360° about acan body as the can body moves along the work path 9.

Any can body 1 that fails an inspection by the full inspection assembly200 is ejected from the work path 9. That is, the fill inspectionassembly 200 includes an ejection assembly 230 that is structured to,and does, eject any deficient can body 1 from the work path 9. As usedherein, >a “deficient” can body 1 is a can body that fails any of theinspections performed by the full inspection assembly 200. Further, inan exemplary embodiment, the full inspection assembly ejection assembly230 is disposed upstream of any processing station 20. As used herein,an ejection assembly disposed upstream relative to all processingstations 20 is an “upstream ejection assembly.” Use of an upstreamejection assembly solves the problems stated above.

As used herein, a “starwheel guide assembly” includes a mountingassembly, a support assembly, and a number of guide rails. The starwheelguide assembly mounting assembly is structured to couple the starwheelguide assembly to a frame assembly, housing assembly, or similarconstruct while positioning the guide rails adjacent an associatedstarwheel. As used herein, a “starwheel guide assembly guide rail” is aconstruct including an elongated and/or extended guide surface that isdisposed a guiding distance from a starwheel. As used herein, a “guidingdistance” means the guiding surface of the guide rail facing anassociated starwheel is spaced a distance from the starwheel so that theguiding surface will not contact a can body temporarily coupled to thestarwheel and will not allow a can body to exit a starwheel pocket 34 ifthe can body disengages from the starwheel. As used herein, a “can bodyheight adjustment assembly” is a sub-assembly of a starwheel guideassembly that is structured to adjust the position of the guide railsrelative to an associated starwheel to accommodate a change in can bodyheight.

As used herein, a “quick-change starwheel guide assembly” means astarwheel guide assembly wherein at least one of the can body heightadjustment assembly and starwheel guide assembly mounting assembly arestructured to be, and/or are, coupled to a starwheel guide assemblymounting base, or similar construct, by an “exceedingly limited numberof couplings.” As used herein, a “quick-change starwheel guide assemblycan body height adjustment assembly” means a can body height adjustmentassembly is structured to be, and/or is, coupled to a starwheel guideassembly support assembly, or similar construct, by an “exceedinglylimited number of couplings.” A “quick-change starwheel guide assemblymounting assembly” means a starwheel guide assembly mounting assemblythat is structured to be, and/or is, coupled to a starwheel guideassembly mounting base, or similar construct, by an “exceedingly limitednumber of couplings.”

As shown in FIGS. 6-9, and as noted above, necker machine 10, includingthe infeed assembly 100 and/or any of the processing stations 20,includes a number of vacuum starwheels 32 as well as a number ofstarwheel guide assemblies 300. Each starwheel guide assembly 300 isassociated with a vacuum starwheel 32 and is structured to maintain acan body 1 in the pockets 34 of that vacuum starwheel 32 at thelocations adjacent the starwheel guide assembly 300. The starwheel guideassemblies 300 are, in an exemplary embodiment, also disposed onselected processing stations 20. That is, the following discussion willaddress a starwheel guide assembly 300 as part of the infeed assembly100, but it is understood that the starwheel guide assemblies 300 arealso associated with the processing stations 20. The starwheel guideassemblies 300 are generally similar and only one is discussed below.

The necker machine 10 (or infeed assembly 100/processing stations 20)include a number of starwheel guide assembly mounting bases 150 that arecoupled, directly coupled, fixed to, or are unitary with, the frameassembly 12. In an exemplary embodiment, each starwheel guide assemblymounting base 150 is disposed adjacent an associated vacuum starwheel32. In an exemplary embodiment, each starwheel guide assembly mountingbase 150 includes an exceedingly limited number of retained couplings152. Use of the exceedingly limited number retained couplings 152 solvesthe problems stated above. Each starwheel guide assembly mounting base150 and an exceedingly limited number retained couplings 152 is alsoidentified as part of the associated starwheel guide assembly 300.

In an exemplary embodiment, the starwheel guide assembly mounting baseretained coupling 152 is selected from the group including, consistingessentially of, or consisting of, tethered fasteners, trapped fasteners(fasteners adjustably fixed to another element so that the trappedfastener is structured to move between a tight position and a looseposition, but cannot move beyond these positions), and expandingcouplings (a body enclosing movable parts with cams structured to movethe movable parts outwardly as the coupling is tightened such as, butnot limited to, the Mitee-Bite Loc-Down® System manufactured byMitee-Bite Products, LLC at P.O. BOX 430, Center Ossipee, N.H. 03814).In an exemplary embodiment, the starwheel guide assembly mounting baseretained coupling 152 includes a locking surface 153.

In an exemplary embodiment, each starwheel guide assembly mounting base150 includes a positioning contour 154. As used herein, a “positioningcontour” 154 means a contour on a first element that is other thangenerally planar, circular, cylindrical, spherical, or symmetrical andwhich is structured to be directly coupled to a second element with nosignificant gaps therebetween having a corresponding “positioningcontour.” For example, a mounting that includes a flat plate with athreaded bore therein does not have a “positioning contour.” That is,another plate coupled by a fastener to the flat plate and the threadedbore can be in many orientations. Conversely, a mounting with atrapezoidal ridge on an otherwise flat plate with a threaded boretherein does have a “positioning contour.” That is, a plate structuredto be coupled thereto has a trapezoidal groove corresponding to thetrapezoidal ridge. Thus, the two plates can only be coupled in aco-planar (immediately adjacent with no significant gap(s)) manner whenthe trapezoidal ridge/groove are aligned with each other. Thus, thecontour orients the two plates relative to each other. Further, when thetwo “positioning contours” are directly coupled, the second element isin a selected position relative to the first element. As used in thedefinition of “positioning contour,” a “selected position” means thatthe second element is only able to be in a single desired position andorientation. For example, on an automobile, a wheel hub and an axle hubhave corresponding contours, typically planar, and four to six lug nutopenings. In this configuration, the wheel can be coupled to the hub inmultiple orientations. As such, the wheel is not limited to a single“selected position” and this configuration does not define a“positioning contour.”

As shown in FIG. 6, in an exemplary embodiment, each starwheel guideassembly mounting base 150 includes a plate 156 including a generallyplanar and generally horizontal upper surface 158 as well as aprotrusion 160. The generally planar upper surface 158 and theprotrusion 160 define a “positioning contour” as defined above.

Each starwheel guide assembly mounting base 150 also includes thestarwheel guide assembly mounting base retained coupling 152. That is,in an exemplary embodiment, each starwheel guide assembly mounting base150 includes an expanding coupling 155. As shown, the upper surface ofeach starwheel guide assembly mounting base protrusion 160 defines acavity (not numbered) in which an expanding coupling 155 is disposed. Inan exemplary embodiment, the expanding coupling 155, or any starwheelguide assembly mounting base retained coupling 152, is elongated andextends generally vertically.

As shown in FIGS. 6-10, each starwheel guide assembly 300 includes astarwheel guide assembly mounting assembly 310, a starwheel guideassembly support assembly 330, a number of starwheel guide assemblyguiderails 350, and a starwheel guide assembly can body heightadjustment assembly 370. In an exemplary embodiment, at least one of thestarwheel guide assembly mounting assembly 310 or the starwheel guideassembly can body height adjustment assembly 370 is a quick-changeassembly. That is, as used herein, “at least one of the starwheel guideassembly mounting assembly 310 or the starwheel guide assembly can bodyheight adjustment assembly 370 is a quick-change assembly” means thateither the starwheel guide assembly mounting assembly 310 is aquick-change starwheel guide assembly mounting assembly 310, as definedabove, or the starwheel guide assembly can body height adjustmentassembly 370 is a quick-change starwheel guide assembly can body heightadjustment assembly 370, as defined above.

The starwheel guide assembly mounting assembly 310 includes a body 312that defines a positioning contour 314. That is, the starwheel guideassembly mounting assembly body positioning contour 314 corresponds tothe starwheel guide assembly mounting base positioning contour 154. Asshown, when the starwheel guide assembly mounting base positioningcontour 154 is a protrusion 160, the starwheel guide assembly mountingassembly positioning contour 314 is a recess 316 that generallycorresponds to the starwheel guide assembly mounting base positioningcontour protrusion 160.

The starwheel guide assembly mounting assembly body 312 also defines a“single active coupling passage” 318. As used herein, a “single activecoupling passage” is a coupling passage that is structured to be usedexclusively to couple two elements. That is, a body with a singlecoupling passage has a “single active coupling passage.” A body with aplurality of coupling passages includes a “single active couplingpassage” when only one of those passages is structured to be used, andis used, to couple two elements together. The starwheel guide assemblymounting assembly single active coupling passage 318 corresponds to thestarwheel guide assembly mounting base retained coupling 152. Thus, whenthe starwheel guide assembly mounting base retained coupling 152 isdisposed on the starwheel guide assembly mounting base positioningcontour protrusion 160, the starwheel guide assembly mounting assemblysingle active coupling passage 318 extends through the starwheel guideassembly mounting assembly positioning contour recess 316. Thus, astarwheel guide assembly mounting assembly body 312 is structured to be,and is, coupled to a starwheel guide assembly mounting base 150 by asingle coupling. This solves the problems identified above. Further, asthe coupling is a retained coupling, this also solves the problemsidentified above. The starwheel guide assembly mounting assembly body312 is also structured to, and does, support an inner guiderail 352,discussed below.

The starwheel guide assembly support assembly 330 is structured to, anddoes, support a number of guiderails; two shown as an inner guiderail352 and an outer guiderail 354, discussed below. The star wheel guideassembly support assembly 330 includes an elongated first support member332 and an elongated second support member 334. The first support member332 and the second support member 334 are collectively identified hereinas, i.e., as used herein, the “starwheel guide assembly support assemblyfirst and second support members” 332, 334. As shown, in an exemplaryembodiment, the starwheel guide assembly support assembly first andsecond support members 332, 334 are generally cylindrical. The starwheelguide assembly support assembly first and second support members 332,334 extend generally horizontally from the starwheel guide assemblymounting assembly body 312 toward the front of the necker machine 10.The starwheel guide assembly support assembly first and second supportmembers 332, 334 are spaced from each other. In an exemplary embodiment,the distal ends of the starwheel guide assembly support assembly firstand second support members 332, 334 include a removable flared cap (notshown) or similar construct that increases the cross-sectional area ofthe distal ends of the starwheel guide assembly support assembly firstand second support members 332, 334.

The number of starwheel guide assembly guiderails 350, in an exemplaryembodiment, includes an inner guiderail 352 and an outer guiderail 354.Each of the starwheel guide assembly inner guiderail 352 (hereinafter,“inner guiderail” 352) and the starwheel guide assembly guiderail outerguiderail 354 (hereinafter, “outer guiderail” 354), includes a body 356,358. Each of the inner guiderail 352 and the outer guiderail 354includes a guide surface 360. As is known, each guide surface 360 iselongated and generally corresponds to the path of travel of a can body1 on a vacuum starwheel 32. That is, each guide surface 360 is generallycurved. The inner guide rail body 356 and the outer guiderail body 358are structured to be, and are, coupled to the starwheel guide assemblysupport assembly 330. In an exemplary embodiment, wherein the starwheelguide assembly support assembly first and second support members 332,334 are generally cylindrical, each of the inner guide rail body 356 andthe outer guiderail body 358 include a pair of spaced, openings (notnumbered) that generally, or substantially, correspond to the starwheelguide assembly support assembly first and second support members 332,334. That is, the pair of spaced >openings are sized, shaped, andpositioned to generally, or substantially, correspond to the starwheelguide assembly support assembly first and second support members 332,334. In an exemplary embodiment, the inner guiderail 352 is coupled,directly coupled, or fixed to the starwheel guide assembly mountingassembly body 312 and moves therewith. The outer guiderail 354 isstructured to be, and is, movably coupled to the starwheel guideassembly support assembly 330.

In an exemplary embodiment, the starwheel guide assembly can body heightadjustment assembly 370 is coupled, directly coupled, fixed, or unitarywith the starwheel guide assembly guiderail outer guiderail body 358 andis identified herein as part of the outer guiderail 354. The starwheelguide assembly can body height adjustment assembly 370 includes aprimary body 372, a secondary body 374, and a single retained coupling376. The starwheel guide assembly can body height adjustment assemblyprimary body 372 defines a single coupling passage 378. The starwheelguide assembly can body height adjustment assembly primary body couplingpassage 378 generally corresponds to the quick-change can body heightadjustment assembly retained coupling 376, discussed below. Thestarwheel guide assembly can body height adjustment assembly primarybody coupling passage 378 further defines a locking surface 379 thatextends generally horizontally. In an exemplary embodiment, thestarwheel guide assembly can body height adjustment assembly primarybody 372 further defines a first support member channel 380 and a secondsupport member channel 382 (collectively, the “starwheel guide assemblycan body height adjustment assembly primary body first and secondchannels” 380, 382), In one embodiment, not shown, the starwheel guideassembly can body height adjustment assembly primary body first andsecond channels 380, 382 each correspond to one of the starwheel guideassembly support assembly first and second support members 332, 334. Asdiscussed below, the starwheel guide assembly support assembly first andsecond support members 332, 334 extend through the starwheel guideassembly can body height adjustment assembly, primary body first andsecond channels 380, 382. In a configuration wherein the starwheel guideassembly can body height adjustment assembly primary body first andsecond channels 380, 382 generally correspond to the starwheel guideassembly support assembly first and second support members 332, 334,there is a possibility that the starwheel guide assembly can body heightadjustment assembly primary body 372 will bind against the starwheelguide assembly support assembly first and second support members 332,334. As such, in another embodiment, the starwheel guide assembly canbody height adjustment assembly primary body first and second channels380, 382 each have a “reduced contact surface.” As used herein, a“reduced contact surface” means two surfaces that do not have asubstantially corresponding contour. In an exemplary embodiment, thestarwheel guide assembly can body height, adjustment assembly primarybody first and second channels 380, 382 are each an inverted generallyV-shaped channel 381, 383. It is understood that an inverted generally Vshaped channel is exemplary and not limiting.

The starwheel guide assembly can body height adjustment assemblysecondary body 374 defines a first engagement surface 390 and a secondengagement surface 392. The starwheel guide assembly can body heightadjustment assembly secondary body first engagement surface 390 and thestarwheel guide assembly can body height adjustment assembly secondarybody second engagement surface 392 are positioned to correspond to thestarwheel guide assembly support assembly first and second supportmembers 332, 334. As used herein, “positioned to correspond” means thatelements are positioned in a similar manner but do not havecorresponding (as defined above) contours. In an exemplary embodiment,each of the starwheel guide assembly can body height adjustment assemblysecondary body first engagement surface 390 and the starwheel guideassembly can body height adjustment assembly secondary body secondengagement surface 392 are generally planar.

The starwheel guide assembly can body height adjustment assemblysecondary body 374 further defines a coupling 384 for the starwheelguide assembly can body height adjustment assembly retained coupling376. The starwheel guide assembly can body height adjustment assemblysecondary body coupling 384, in an exemplary embodiment, is a threadedbore. The starwheel guide assembly can body height adjustment assemblyretained coupling 376 is adjustably fixed to the starwheel guideassembly can body height adjustment assembly secondary body 374. Thatis, as shown, the starwheel guide assembly can body height adjustmentassembly retained coupling 376 is in one embodiment (not shown) atrapped coupling at the starwheel guide assembly can body heightadjustment assembly secondary body coupling 384. Further, the starwheelguide assembly can body height adjustment assembly secondary body 374 ismovably coupled to the starwheel guide assembly can body heightadjustment assembly primary body 372 with the starwheel guide assemblycan body height adjustment assembly retained coupling 376 extendingthrough the starwheel guide assembly can body height adjustment assemblyprimary body coupling passage 378 with the starwheel guide assembly canbody height adjustment assembly retained coupling 376 structured toengage the starwheel guide assembly can body height adjustment assemblyprimary body coupling passage locking surface 379.

Each starwheel guide assembly 300 is assembled as follows. The starwheelguide assembly mounting assembly 310 and the starwheel guide assemblysupport assembly 330 are coupled, directly coupled, or fixed to eachother, or are formed as a unitary body. The starwheel guide assembly canbody height adjustment assembly 370 is coupled, directly coupled, orfixed to the outer guiderail 354. It is understood that the innerguiderail 352 and the outer guiderail 354 are oriented so that theirguide surfaces 360 extend generally parallel to each other. The outerguiderail 354 is then movably coupled to the starwheel guide assemblysupport assembly 330 with the starwheel guide assembly support assemblyfirst support member 332 disposed between the quick-change can bodyheight adjustment assembly primary body first support member channel 380and the quick-change can body height adjustment assembly secondary bodyfirst engagement surface 390, and, the starwheel guide assembly supportassembly second support member 334 disposed between the quick-change canbody height adjustment assembly primary body second support memberchannel 382 and the quick-change can body height adjustment assemblysecondary body second engagement surface 392. In this configuration,each quick-change starwheel guide assembly 300 is a “unit assembly.” Asused herein, a “unit assembly” is an assembly of a plurality of elementsthat are coupled together as a unit. That is, the elements of a “unitassembly” can be collectively moved from one location to another. Thus,each starwheel guide assembly 300, with the exception of the starwheelguide assembly mounting base 150, are structured to be removed from thenecker machine 10 and replaced with another starwheel guide assembly300, as discussed below.

The starwheel guide assembly can body height adjustment assembly 370operates as follows. Initially, it is assumed that the starwheel guideassembly can body height adjustment assembly 370 is set for a can body 1of a first height. That is, the outer guiderail guide surfaces 360 is ata guiding distance relative to a can body 1 of a first height. In thisconfiguration, the quick-change can body height adjustment assemblyretained coupling 376 is in a second position wherein the quick-changecan body height adjustment assembly secondary body first engagementsurface 390 and the quick-change can body height adjustment assemblysecondary body second engagement surface 392 engage an associatedstarwheel guide assembly support assembly support first or second member332, 334. That is, the quick-change can body height adjustment assemblyretained coupling 376 is manipulated to draw the starwheel guideassembly can body height adjustment assembly secondary body 374 towardthe starwheel guide assembly can body height adjustment assembly primarybody 372. The friction between the starwheel guide assembly can bodyheight adjustment assembly primary body first and second channels 380,382 and the starwheel guide assembly support assembly support first orsecond member 332, 334, as well as the friction between the quick-changecan body height adjustment assembly secondary body first engagementsurface 390, the quick-change can body height adjustment assemblysecondary body second engagement surface 392 and the starwheel guideassembly support assembly support first or second member 332, 334,maintain the starwheel guide assembly can body height adjustmentassembly 370, and therefore the outer guiderail 354, in a selectedlocation.

When the position of the outer guiderail 354 needs to be adjusted toaccommodate a can body 1 of a second height, the quick-change can bodyheight adjustment assembly retained coupling 376 is moved to a firstposition wherein the starwheel guide assembly can body height adjustmentassembly secondary body 374 moves away from the starwheel guide assemblycan body height adjustment assembly primary body 372. In thisconfiguration, the starwheel guide assembly can, body height adjustmentassembly 370, and therefore the outer guiderail 354, are movablelongitudinally along the first and second support members 332, 334. Thisadjusts the position of the outer guiderail 354 so as to be at a guidingdistance relative to the can body 1 of a second height.

Stated alternately, each quick-change can body height adjustmentassembly secondary body 374 moves between a non-engaging first position,wherein each quick-change can body height adjustment assembly secondarybody first engagement surface 390 and each quick-change can body heightadjustment assembly secondary body second engagement surface 392 do notengage an associated starwheel guide assembly support assembly first andsecond support member 332, 334, and an engaging second position, whereineach quick-change can body height adjustment assembly secondary bodyfirst engagement surface 390 and each quick-change can body heightadjustment assembly secondary body second engagement surface 392 engagean associated starwheel guide assembly support assembly first and secondsupport member 332, 334.

The starwheel guide assembly can body height adjustment assembly 370moves between a first and second configuration corresponding to thefirst and second, position of the quick-change can body heightadjustment assembly secondary body 374. Moreover, the starwheel guideassembly can body height adjustment assembly 370 moves between the firstand second configurations via adjusting the single quick-change can bodyheight adjustment assembly retained coupling 376. This solves theproblems stated above.

The starwheel guide assembly mounting assembly 310 operates as follows.When installed, the starwheel guide assembly mounting assembly bodypositioning contour 314 is directly coupled to the starwheel guideassembly mounting base positioning contour 154. In this position, thestarwheel guide assembly mounting base retained coupling 152 extendsthrough the starwheel guide assembly can body height adjustment assemblyprimary body coupling passage 378. Further, the starwheel guide assemblymounting base retained coupling locking surface 153 engages thestarwheel guide assembly can body height adjustment assembly primarybody coupling passage locking surface 379. In this configuration, thestarwheel guide assembly mounting assembly 310, and therefore thestarwheel guide assembly 300, is fixed to the necker machine 10 and/orthe frame assembly 12. Hereinafter, this configuration is identified asthe “second configuration” of the starwheel guide assembly mountingassembly 310.

Each starwheel guide assembly mounting assembly 310 is structured toposition the guide surfaces 360 of the inner guiderail 352 and the outerguiderail 354 at a guiding distance relative to a can body 1 of a firstdiameter. When the necker machine 10 needs to process a can body of asecond diameter, each starwheel guide assembly 300 needs to be replaced.To do this, the starwheel guide assembly mounting base retained coupling152 is manipulated so that the starwheel guide assembly mounting baseretained coupling locking surface 153 does not engage the starwheelguide assembly can body height adjustment assembly primary body couplingpassage locking surface 379. In this configuration, hereinafter, the“first configuration” of the starwheel guide assembly mounting assembly310, the starwheel guide assembly 300 is structured to be, and is,removed from the associated starwheel guide assembly mounting base 150.The starwheel guide assembly 300 is then replaced with another, orreplacement, starwheel guide assembly 300 sized to accommodate a canbody 1 of a second diameter. It is noted that the starwheel guideassembly 300 is removed as a unit because the starwheel guide assembly300 is a unit assembly.

Installation of the replacement starwheel guide assembly 300 includespositioning the replacement starwheel guide assembly mounting, assemblybody positioning contour 314 over the starwheel guide assembly mountingbase positioning contour 154. This further positions the starwheel guideassembly mounting base retained coupling 152 in the replacementstarwheel guide assembly mounting assembly single active couplingpassage 318. The starwheel guide assembly mounting base retainedcoupling 152 is manipulated so that the starwheel guide assemblymounting base retained coupling locking, surface 153 engages thestarwheel guide assembly can body height adjustment assembly primarybody coupling passage locking surface 379.

Accordingly, the starwheel guide assembly 300 is installed/removed as aunit because the starwheel guide assembly 300 is a unit assembly.Further, because the starwheel guide assembly mounting assembly 310and/or the can body height adjustment assembly 370 are a quick-changeassemblies (each have a single relevant coupling), and, because thecouplings are retained couplings, the problems identified above aresolved.

As shown in FIGS. 11-14, the quick-change starwheel guide assemblyconcept is, in an exemplary embodiment, also incorporated into aquick-change vacuum starwheel assembly 400. As used herein, a“quick-change vacuum starwheel assembly” 400 means a vacuum starwheelassembly that includes at least one of a quick-change height adjustmentassembly 550 or a quick-change vacuum starwheel mounting assembly 800.As used herein, a “quick-change can body height adjustment assembly” 550means a construct structured to move a vacuum starwheel 32 axially on anassociated rotating shaft wherein only a very limited number of retainedcouplings are required to be loosened or removed so as to allow theaxial movement of the starwheel. As used herein, a “quick-change vacuumstarwheel mounting assembly” 800 means a mounting assembly structured tocouple, directly couple, or fix the separable vacuum starwheelcomponents to a rotating shaft via one of a limited number of couplings,a very limited number of couplings, or an exceedingly limited number ofcouplings. In the definition of “quick-change vacuum starwheel mountingassembly” 800, the term “couplings” means a coupling that is structuredto be secured/tightened such as, but not limited to a bolt on a threadedrod, and does not include an unsecured coupling such as, but not limitedto, a lug extending through a passage.

In an exemplary embodiment, the quick-change vacuum starwheel assembly400 includes a rotating shaft assembly 410, a vacuum starwheel bodyassembly 450, a vacuum assembly 480, a quick-change height adjustmentassembly 550 and a quick-change vacuum starwheel mounting assembly 800.The rotating shaft assembly 410 includes a housing assembly 412, amounting disk 414 and a rotating shaft 416. The rotating shaft assemblyhousing assembly 412 is a housing that is structured to be, and is,disposed about the rotating shaft assembly rotating shaft 416. Therotating shaft assembly housing assembly 412 is structured to be, andis, coupled, directly coupled, or fixed to the frame assembly 12. Thus,the rotating shaft assembly housing assembly 412 is in a fixed locationrelative to the frame assembly 12. The rotating shaft assembly rotatingshaft 416 is operatively coupled to the drive assembly 2000 and is alsoidentified as a part thereof. The drive assembly 2000 is structured to,and does, impart a rotational motion to the rotating shaft assemblyrotating shaft 416 so that the rotating shaft assembly rotating shaft416 rotates about its longitudinal axis.

In an exemplary embodiment, the rotating shaft assembly rotating shaft416 includes a generally cylindrical body 418 having a proximal end 420adjacent the frame assembly 12 and a distal end 422 spaced from theframe assembly 12. The rotating shaft assembly rotating shaft body 418,as shown in the Figures, includes portions with different radii.Further, in an exemplary embodiment, selected portions of the rotatingshaft assembly rotating shaft body 418 define bearing surfaces and/orsurfaces structured to support a bearing, as discussed below.

The rotating shaft assembly rotating shaft body distal end 422 includesa traveler hub mounting 424 (hereinafter, “traveler hub mounting 424”).The traveler hub mounting 424 is structured to be, and is, coupled to atraveling hub assembly 570, discussed below. In an exemplary embodiment,the traveler hub mounting 424 includes a central cavity 426 and twolongitudinal slots, i.e., a first longitudinal slot 428 and a secondlongitudinal slot 430, as well as a number of coupling components (notshown/numbered). Further, the traveler hub mounting central cavity 426includes a rotational coupling cavity 427 disposed on the rotating shaftassembly rotating shaft 416 axis of rotation. In an exemplaryembodiment, the coupling components (not shown/numbered) are threadedbores disposed on the axial surface of the rotating shaft assemblyrotating shaft body distal end 422. Further, in an exemplary embodiment,the rotating shaft assembly rotating shaft distal end 422 includes apositioning key mounting 432 (hereinafter, “rotating shaft assemblypositioning key mounting 432”). As shown, the rotating shaft assemblypositioning key mounting 432 is, in one embodiment, a longitudinalgroove 434,

The vacuum starwheel body assembly 450 generally defines a vacuumstarwheel 32 as defined above. That is, a vacuum starwheel 32 includes atorus-like assembly with a plurality of pockets 34 disposed on theradial surface thereof. As is known, a vacuum starwheel body assembly450, or the parts thereof, are often moved, carried, and positioned, bya human without the use of a cart or similar construct. Thus, dependingupon the size of the vacuum starwheel body assembly 450, the vacuumstarwheel body assembly 450 includes a number of vacuum starwheel bodyassembly body segments 452. In an exemplary embodiment, the vacuumstarwheel body assembly body segments 452 are substantially similar anddefine an equal portion of the vacuum starwheel 32. That is, forexample, if a vacuum starwheel body assembly 450 includes two vacuumstarwheel body assembly body segments 452 (not shown), each starwheelbody assembly body segment 452 is generally semi-circular and defines ahalf of the disk-like body. That is, there are two vacuum starwheel bodyassembly body segments 452 each defining an outer surface that extendsabout 180°. In the embodiment shown in the Figures, the vacuum starwheelbody assembly 450 includes four starwheel body assembly body segments452. The four starwheel body assembly body segments 452 are generallysimilar and each defines, generally, a quarter of a circle. That is, inthis embodiment, each starwheel body assembly body segment 452 includesan outer surface 454 that defines an arc of about 90°.

As each starwheel body assembly body segment 452 is generally similar,only one is described herein. Each starwheel body assembly body segment452 defines, generally, a 90° generally circular arc. That is, eachstarwheel body assembly body segment 452 extends over an arc of about90°. Each starwheel body assembly body segment 452 includes>an axialmounting portion 462 and a peripheral pocket portion 464. In oneexemplary embodiment, each starwheel body assembly body segment 452 is aunitary body. In another embodiment, as shown, the axial mounting,portion 462 and the peripheral pocket portion 464 are separate bodiesthat are coupled, directly coupled, or fixed together by fasteners 460.

The starwheel body assembly body segment axial mounting portion 462includes a generally planar, generally arcuate body 461. In an exemplaryembodiment, the starwheel body assembly body segment axial mountingportion 462 defines three mounting passages; a retained coupling passage466, a first lug passage 468, and a second lug passage 469 (hereinafter,and collectively “starwheel body assembly body segment axial mountingportion passages 466, 468, 469”). The starwheel body assembly bodysegment axial mounting portion passages 466, 468, 469 extend generallyperpendicular to the plane of the starwheel body assembly body segmentaxial mounting portion 462. The starwheel body assembly body segmentaxial mounting portion 462 (and therefore the vacuum starwheel bodyassembly 450) is also identified herein as part of the quick-changevacuum starwheel mounting assembly 800.

The starwheel body assembly body segment peripheral pocket portion 464defines a number of pockets 34 on the radial surface of the starwheelbody assembly body segment 452. As discussed above, each starwheel bodyassembly body segment peripheral pocket portion pocket 34 (hereinafter,“starwheel body assembly body segment peripheral pocket 34” or“starwheel pocket 34”) defines a generally semi-cylindrical cradle sizedto correspond to a can body 1 or can bodies of generally similar radii.Each starwheel body assembly body segment peripheral pocket 34 includesa radially extending passage 470 that extends through the starwheel bodyassembly body segment peripheral pocket portion 464. Each starwheel bodyassembly body segment peripheral pocket passage 470 is structured to be,and is, in fluid communication with the vacuum assembly 480 and apartial vacuum (or suction) is drawn therethrough.

Further, the starwheel body assembly body segment peripheral pocketportion 464 is thicker (in a direction perpendicular to the plane ofstarwheel body assembly body segment axial mounting portion body 461)than the starwheel body assembly body segment axial mounting portionbody 461. The starwheel body assembly body segment peripheral pocketportion 464 also extends a greater distance rearwardly (toward the frameassembly 12) as opposed to a greater, or equal, distance forwardly (awayfrom the frame assembly 12). In this configuration, and when allstarwheel body assembly body segments 452 are coupled to form a vacuumstarwheel 32, the starwheel body assembly body segments 452 define agenerally cylindrical, or disk-like, cavity 472 (hereinafter, the“starwheel body cavity” 472). The starwheel body cavity 472 is in fluidcommunication with the vacuum assembly 480 as discussed below.

Further, the inner side (the side generally facing the frame assembly12) of the starwheel body assembly body segment peripheral pocketportion 464 defines a sealing surface 474 (hereinafter, the “starwheelbody assembly body sealing surface” 474). In an exemplary embodiment,the starwheel body assembly body sealing surface 474 is generallycircular and has the same radius (hereinafter, the “starwheel bodyassembly body sealing surface radius”) regardless of the size of thevacuum starwheel body assembly 450. For example, a first vacuumstarwheel body assembly 450 has a radius of twenty-four inches and thestarwheel body assembly body sealing surface 474 has a radius oftwenty-two inches. A second vacuum starwheel body assembly 450 has aradius of twenty-six inches while the starwheel body assembly bodysealing surface 474 still has a radius of twenty-two inches. To ensurethe second vacuum starwheel body assembly 450 has a starwheel bodyassembly body sealing surface radius of twenty-two inches, the radiallyextending thickness of the starwheel body assembly body segmentperipheral pocket portion 464 is increased by about two inches.

Further, it is understood that different vacuum starwheel bodyassemblies 450 have different configurations. For example, a firstvacuum starwheel body assembly 450, as shown, has a first radius andincludes twenty starwheel pockets 34 each with a first pocket radius. Asecond vacuum starwheel body assembly not shown, has a similar radius,but includes sixteen starwheel pockets 34 with a larger, second pocketradius. A third vacuum starwheel body assembly, not shown, has a greaterradius and twenty-four starwheel pockets 34 with a first pocket radius.Thus, the vacuum starwheel body assemblies 450 are structured to beexchanged so as to accommodate can bodies 1 of different radii and/or asneeded to accommodate desired operational characteristics of the neckermachine 10 such as, but not limited to, the processing speed as measuredin cans per minute,

As shown in FIGS. 15-16, the vacuum assembly 480 includes a telescopingvacuum conduit 484, a vacuum housing assembly 486 and a vacuum sealassembly 540. The vacuum assembly 480 is structured to be in, and is in,fluid communication with a vacuum generator 482 (shown schematically).As is known, the vacuum generator 482 is coupled to, and structured toreduce the fluid/air pressure in a plurality of vacuum starwheels 32. Itis understood that the term “vacuum” is used generally to mean asubstantially reduced pressure relative to the atmosphere and does notrequire an absolute vacuum. The vacuum generator 482 is structured to,and does, substantially reduce the fluid/air pressure in the vacuumassembly vacuum housing assembly 486 and elements in fluid communicationtherewith. While not specifically included in the vacuum assembly 480,the interaction of the vacuum generator 482 and the vacuum assembly 480means that, as used herein, the vacuum assembly 480 is structured togenerate a vacuum. Further, as used herein, a statement that the vacuumassembly 480 “is in fluid communication” with another element means thata fluid path exists between the vacuum assembly 480 and the element andthat suction is applied to, or through, the element. For example, thevacuum assembly 480 is, selectively, in fluid communication with eachstarwheel body assembly body segment peripheral pocket 34. Thus, eachstarwheel body assembly body segment peripheral pocket 34 has a vacuumapplied thereto and there is suction through each starwheel bodyassembly body segment peripheral pocket passage 470.

The vacuum assembly telescoping vacuum conduit 484 includes a number oftelescoping bodies 490, 492 (two shown). The vacuum assembly telescopingvacuum conduit telescoping bodies 490, 492 are structured to be, andare, disposed in a telescoping configuration. As used herein, two bodiesin a “telescoping configuration” means that one body has a smaller, butcorresponding, cross-sectional shape relative to a larger body and thesmaller body is movably disposed within the larger body and structuredto move between a retracted position, wherein the smaller body issubstantially disposed within the larger body, and an extended position,wherein the smaller body substantially extends from the larger body.Further, in an exemplary embodiment, the vacuum assembly telescopingvacuum conduit 484 includes a seal between the two vacuum assemblytelescoping vacuum conduit telescoping bodies 490, 492.

As shown in FIGS. 17-19, the vacuum assembly vacuum housing assembly 486includes a body 500 defining a vacuum chamber 502. In an exemplaryembodiment, the vacuum assembly vacuum housing assembly body 500includes a generally concave and generally arcuate portion 504, amovable mounting portion 506 and a front plate portion 508. The vacuumassembly vacuum housing assembly arcuate portion 504 defines an outletpassage 510. The vacuum assembly vacuum housing assembly arcuate portionoutlet passage 510 is coupled, directly coupled, or fixed to the vacuumassembly telescoping vacuum conduit 484 and is in fluid communicationtherewith. In an exemplary embodiment, the vacuum assembly vacuumhousing assembly movable mounting portion 506 is a generally planar body516 that is coupled, directly coupled, or fixed to the vacuum assemblyvacuum housing assembly arcuate portion 504. The vacuum assembly vacuumhousing assembly movable mounting portion body 516 defines a rotating,shaft passage 518 and two sliding mount passages 520, 522. A number ofbearings 524 such as, but not limited to radial bearings 578(hereinafter, traveling hub assembly radial bearing” 578 discussedbelow), are disposed about the vacuum assembly vacuum housing assemblymovable mounting portion body rotating shaft passage 518 and arestructured to be, and are, disposed between and coupled to both thevacuum assembly vacuum housing assembly movable mounting portion body516 and the rotating shaft assembly rotating shaft 416,

The vacuum assembly vacuum housing assembly front plate portion 508includes a generally planar body 530 (or assembly of generally planarbodies) and defines an inlet passage 512 and a generally circularrotating shaft passage 532. The vacuum assembly vacuum housing assemblyfront plate portion planar body 530 is coupled, directly coupled, orfixed to the vacuum assembly vacuum housing assembly arcuate portion 504and the vacuum assembly vacuum housing, assembly front plate portioninlet passage 512 is in fluid communication with the vacuum assemblyvacuum housing assembly arcuate portion outlet passage 510. When coupledto the rotating shaft assembly 410, as described below, the plane of thevacuum assembly vacuum housing assembly front plate portion planar body530 extends substantially perpendicular to the rotating shaft assemblyrotating shaft 416 axis of rotation.

Further, the vacuum assembly vacuum housing assembly front plate portion508 includes a baffle assembly 536 (hereinafter, “vacuum housingassembly baffle assembly 536”). The vacuum housing assembly baffleassembly 536 is structured to, and does, substantially obstruct fluidcommunication between the vacuum generator 482 and the starwheel pocketradially extending passage 470 at selected locations. That is, asdescribed below, the vacuum starwheel 32 rotates and the starwheelpocket radially extending passage 470 moves in a circular motion aboutthe vacuum assembly vacuum housing assembly front plate portion 508. Thevacuum housing assembly baffle assembly 536 is disposed adjacent thepath of travel of the starwheel pockets 34 and substantially obstructfluid communication between the vacuum generator 482 and the starwheelpocket radially extending passage 470. This, in effect, precludes anysubstantial suction being applied through the starwheel pocket radiallyextending passage 470 adjacent the baffle assembly 536. As is known, atlocations along the path of travel of the starwheel pockets 34 whereinthe vacuum generator 482 is in fluid communication with the starwheelpocket radially extending passage 470, a can body 1 disposed in astarwheel pocket 34 is maintained in the starwheel pocket 34 via thesuction applied to the starwheel pocket 34. At locations adjacent thevacuum housing assembly baffle assembly 536, the suction is eliminated,or substantially reduced, whereby a can body 1 disposed in a starwheelpocket 34 is not maintained in the starwheel pocket 34. That is, at thevacuum housing assembly baffle assembly 536, the can bodies 1 arereleased from the starwheel pocket 34 and are able to move to anothervacuum starwheel 32, a non-vacuum starwheel 24, or other constructstructured to support a can body 1.

The vacuum seal assembly 540 is coupled, directly coupled, or fixed tothe forward face (the side away from the frame assembly 12) of thevacuum assembly vacuum housing assembly front plate, portion 508. Thevacuum seal assembly 540 includes a seal body 542 that is generallycircular and which has about the same radius as the starwheel bodyassembly body sealing surface 474. In this configuration, the vacuumseal assembly body 542 is structured to, and does, sealingly engage thestarwheel body assembly body sealing surface 474. As used herein,“sealingly engage” means to contact in a manner so as to resist thepassage of a fluid. As noted above, the term “vacuum” means a volumewith a reduced pressure relative to the atmosphere and does not requirean absolute vacuum. As such, the interface of the vacuum seal assemblybody 542 and the starwheel body assembly body sealing surface 474 isstructured to, and does, resist the passage of air; some passage of airis, however, permitted. Accordingly, the vacuum seal assembly body 542is not required to form a leak-proof seal and is, in an exemplaryembodiment, made from a fabric such as, but not limited to felt. As feltis an inexpensive material, this solves the problems stated above.

Further, as detailed below, the vacuum seal assembly 540, i.e., thevacuum seal assembly body 542, is a “lateral scratch resistant seal”541. In the prior art, wherein a vacuum seal is disposed adjacent theinner radial surface of a starwheel body assembly body segmentperipheral pocket portion 464, removal/adjustment of the vacuumstarwheel 32 caused the vacuum starwheel 32 to move longitudinally alongthe rotating shaft assembly rotating shaft 416 to move laterally acrossthe seal. This could damage the seal. In the configuration disclosedabove, the sealing surface of the vacuum seal assembly body 542 (thesurface that seals against the starwheel body assembly 450) is an axialsurface relative to the rotating shaft assembly rotating shaft 416.Thus, when the vacuum starwheel 32 is moved longitudinally along therotating shaft assembly rotating shaft 416, the vacuum starwheel 32moves in a direction normal to the sealing surface of the vacuum sealassembly body 542. That is, the vacuum starwheel 32 does not move acrossthe vacuum seal assembly 540, i.e., the vacuum seal assembly body 542.As used herein, a seal that is positioned so that the element againstwhich it seals moves in a direction normal to the sealing surface of theseal is a “lateral scratch resistant seal.”

Elements of the vacuum assembly 480 are also identified herein as partof the quick-change height adjustment assembly 550 and/or thequick-change vacuum starwheel mounting assembly 800, as discussed below.

As shown in FIG. 11, the quick-change vacuum starwheel assembly 400 alsoincludes a guide assembly 300A structured to maintain a can body 1 inthe pockets 34 of an associated vacuum starwheel 32 at the locationsadjacent the starwheel guide assembly 300A. Similar to the starwheelguide assemblies 300 described above, a quick-change vacuum starwheelassembly guide assembly 300A includes a number of guiderails 350A(reference number 350A identifies the quick-change vacuum starwheelassembly guiderails collectively); four shown as a first inner guiderail352A, a second inner guiderail 353A, a first outer guiderail 354A, and asecond outer guiderail 355A. Each quick-change vacuum starwheel assemblyguide assembly guiderails 350A includes a guide surface 360A.

Each pair of the quick-change vacuum starwheel assembly guiderails 350includes a mounting block; an inner guiderail mounting block 660 and anouter guiderail mounting block 662. Each guiderail mounting block 660,662 includes two retained couplings 664. The first inner guiderail 352Aand second inner guiderail 353A are each coupled, directly coupled, orfixed to the inner guiderail mounting block 660 by a single retainedcoupling 664. The inner guiderail mounting block 660 is coupled,directly coupled, or fixed to the quick-change vacuum starwheel heightadjustment assembly base assembly fixed base member 562. The first outerguiderail 354A and the second outer guiderail 355A are each coupled,directly coupled, or fixed to the outer guiderail mounting block 662 bya single retained coupling 664. The outer guiderail mounting block 662is coupled, directly coupled, or fixed to the quick-change vacuumstarwheel height adjustment assembly base assembly movable base member564 and moves therewith. Further, the elements discussed in thisparagraph are also identified as elements of the quick-change vacuumstarwheel mounting assembly 800.

The quick-change vacuum starwheel assembly guide assembly 300A is alsoidentified herein as part of the quick-change height adjustment assembly550 and/or the quick-change vacuum starwheel mounting assembly 800, asdiscussed below.

As noted above, the quick-change height adjustment assembly 550 means aconstruct structured to move a vacuum starwheel 32 axially on anassociated starwheel shaft wherein only a very limited number, or anexceedingly limited number, of retained couplings, are required to beloosened or removed so as to allow the axial movement of the starwheel.In an exemplary embodiment, the very limited number, or exceedinglylimited number, of retained couplings are a very/exceedingly limitednumber of quick-change height adjustment assembly retained releasecouplings 552, discussed below.

As shown in FIGS. 17-19, in an exemplary embodiment, the quick-changeheight adjustment assembly 550 includes a base assembly 560 (which isalso described herein as the vacuum assembly vacuum housing assemblymovable mounting portion 506) and a traveling hub assembly 570. Thequick-change height adjustment assembly base assembly 560 includes afixed base member 562, a movable base member 564, and a number ofelongated support members 566. The quick-change vacuum starwheel heightadjustment assembly base assembly fixed base member 562 is structured tobe, and is, fixed to the rotating shaft assembly housing assembly 412.The quick-change vacuum starwheel height adjustment assembly baseassembly fixed base member 562 also defines two support member passages563 that correspond to the quick-change vacuum starwheel heightadjustment assembly base assembly elongated support members 566. Thequick-change vacuum starwheel height adjustment assembly base assemblyelongated support members 566 are movably coupled to the quick-changevacuum starwheel height adjustment assembly base assembly fixed basemember 562. The quick-change vacuum starwheel height adjustment assemblybase assembly elongated support members 566 extend generallyhorizontally.

The quick-change vacuum starwheel height adjustment assembly baseassembly movable base member 564 is structured to be, and is, fixed tothe quick-change vacuum starwheel height adjustment assembly baseassembly elongated support members 566 and is structured to, and does,move longitudinally thereon.

The quick-change height adjustment assembly traveling hub assembly 570(hereinafter, “traveling hub assembly 570”) includes a base 572, anactuator 574, a traveler assembly 576, a radial bearing 578, and apositioning key assembly 580. The traveling hub assembly base 572 isstructured to be, and is, coupled, directly coupled, or fixed to therotating shaft assembly rotating shaft 416. That is, the traveling hubassembly base 572 rotates with the rotating shaft assembly rotatingshaft 416. The traveling hub assembly base 572, as shown, includes abody 581 defining a generally circular, central opening (not shown) anda number of coupling or fastener passages. As shown, fasteners 582extend through the traveling, hub assembly base body 581 and are coupledto the threaded bores disposed on the axial, surface of the rotatingshaft assembly rotating shaft body distal end 422.

In an exemplary embodiment, the traveling hub assembly actuator 574 is ajackscrew 590 and has a threaded body 592 with a first end 594 and asecond end 596. This single traveling hub assembly actuator, orexceedingly limited number of traveling hub assembly actuators 574, isthe only actuator structured to move the quick-change height adjustmentassembly 550 and associated elements on the rotating shaft assemblyrotating shaft 416. The traveling hub assembly actuator body first end594 defines a coupling such as, but-riot limited to, a hex-head lug 598.As is known, a hex-head lug 598 is structured to be operatively coupledto a manual actuator such as, but, not limited to, a wrench. Further,the traveling hub assembly actuator, body first end 594 includes aflange 600. The portion of the traveling hub assembly actuator bodyfirst end 594 between the traveling hub assembly actuator body hex-headlug 598 and the traveling hub assembly actuator body flange 600 is sizedto correspond to and to be rotatably disposed in, and which is rotatablydisposed in, the traveling hub assembly base 572 central opening. Inthis configuration, the traveling hub assembly actuator 574 is trappedin the traveling hub assembly base 572. The traveling hub assemblyactuator body second end 596 defines a rotatable mounting 602 that isstructured to be, and is, rotatably coupled to the traveler hub mountingcentral cavity rotational coupling cavity 427.

The traveling hub assembly traveler assembly 576 (hereinafter, “travelerassembly 576”) includes a traveler bracket 610, a generally cylindricaltraveler collar 620, and a generally disk-like traveler mounting 630.The traveling hub assembly traveler assembly traveler bracket 610(hereinafter, “traveler bracket 610”) includes a body 612 defining athreaded central passage 614 and two opposed radially extending arms616, 617. The traveler assembly traveler bracket central passage 614threads are structured to, and do, correspond to the threads of thetraveling hub assembly actuator 574. Each of the traveler bracket bodyarms 616, 617 define a passage 618 for a fastener 619.

The traveler assembly collar 620 includes generally cylindrical body 622defining a central passage 624 sized to correspond to the rotating shaftassembly rotating shaft 416 as well as a positioning key mounting 626.As shown, and in an exemplary embodiment, the traveler assembly collaris a generally hollow cylindrical body 622. The traveler assembly collarbody 622 includes threaded bores (not numbered) on the front axialsurface. In an exemplary embodiment, the traveler assembly collar 620 isa split body 621. That is, a “split body” means a generally hollow,cylindrical body with an axially extending, i.e., longitudinallyextending, gap 623. The traveler assembly collar body 622 furtherincludes an exceedingly limited number of retained release couplings 625(which is one of the quick-change height adjustment assembly retainedrelease couplings 552) extending across the traveler assembly collarbody gap 623. The traveler assembly collar body retained releasecoupling 625 moves between two configurations, a loose, firstconfiguration wherein the opposing sides of the traveler assembly collarbody 622 are separated (and wherein the traveler assembly collar bodycentral passage 624 loosely corresponds to the rotating shaft assemblyrotating shaft 416), and, a secure/tight second configuration whereinthe opposing sides of the traveler assembly collar body 622 are drawntogether (and wherein the traveler assembly collar body central passage624 snuggly corresponds to the rotating shaft assembly rotating shaft416). Thus, when the traveler assembly collar body retained releasecoupling 625 is in the first configuration, the traveler assembly collarbody 622 is in a corresponding first configuration wherein the travelerassembly collar body 622 is movably coupled, or not fixed, to therotating shaft assembly rotating shaft 416, and, when the travelerassembly collar body retained release coupling 625 is in the secondconfiguration, the traveler assembly collar body 622 is in a tight,second configuration wherein the traveler assembly collar body 622 isfixed to the rotating shaft assembly rotating shaft 416.

As shown in FIG. 14, the traveler assembly traveler mounting 630 is, inan exemplary embodiment, a generally planar disk-like body 632, or anassembly of bodies that form a disk-like body 632, disposed about, andcoupled, directly coupled, or fixed to, the traveler assembly collar620. In another embodiment, the traveler assembly collar 620 and thetraveler assembly traveler mounting 630 are unitary. The travelerassembly traveler mounting body 632 includes a mounting surface 634which, as shown, is the front surface of the traveler assembly travelermounting body 632 (i.e., the side away from the frame assembly 12). Thetraveler assembly traveler mounting body mounting surface 634 includes anumber of retained couplings 636 (as defined above) and a number of setsof alignment lugs (designated in the Figures as a first alignment lug638 and a second alignment lug 640). That is, there is one group ofretained couplings 636 and alignment lugs 638, 640 for each vacuumstarwheel body assembly body segment 452. The traveler assembly travelermounting body mounting surface lugs 638, 640 are not threaded orotherwise structured to couple elements and are not, as used herein,“couplings.”

In an exemplary embodiment, the traveler assembly traveler mounting bodymounting surface alignment lugs 638, 640 (hereinafter, “travelerassembly traveler mounting body lugs 638, 640”) and the travelerassembly traveler mounting body mounting surface retained couplings 636(hereinafter, “traveler assembly traveler mounting body retainedcoupling(s) 636”) are disposed in a pattern corresponding to thepositions of the starwheel body assembly body segment axial mountingportion passages 466, 468, 469. As shown in the Figures, and in anexemplary embodiment, the traveling hub assembly alignment lugs 638, 640and the traveler assembly traveler mounting body retained coupling 636are disposed in groups with one traveling hub assembly alignment lug638, 640 disposed on each side of a traveler assembly traveler mountingbody retained coupling 636. Further, the traveler assembly travelermounting body lugs 638, 640 and the associated traveler assemblytraveler mounting body retained coupling 636 are disposed along an arc.In the embodiment shown, there are four groups of a traveler assemblytraveler mounting body retained coupling 636 and two traveler assemblytraveler mounting body lugs 638, 640. That is, each of the four groupsof a traveler assembly traveler mounting body retained coupling 636 andtwo traveler assembly traveler mounting body lugs 638, 640 arestructured to be, and are, coupled, directly coupled, or fixed to one ofthe four vacuum starwheel body assembly body segments 452. It isunderstood that the starwheel body assembly body segment axial mountingportion passages 466, 468, 469 are disposed in a similar pattern. Thatis, the starwheel body assembly body segment axial mounting portionfirst lug passage 468 and the starwheel body assembly body segment axialmounting portion second lug passage 469 are disposed on either side ofthe starwheel body assembly body segment axial mounting portion retainedcoupling passage 466 and along an arc.

The traveling hub assembly radial bearing 578 is structured to be, andis, coupled or fixed to both the vacuum assembly 480 and the vacuumstarwheel body assembly 450. In an exemplary embodiment, shown in FIG.12, the traveling hub assembly radial bearing 578 includes two races; aninner race 650 and an outer race 652. As is known, bearing elements 654are movably disposed between the races 650, 652. The traveling hubassembly radial bearing inner race 650 is fixed to the vacuum assembly480 and the traveling hub assembly radial bearing outer race 652 isfixed to the vacuum starwheel body assembly 450. More specifically, asshown, the traveling hub assembly radial bearing outer race 652 is fixedto the traveler assembly collar 620 which, as detailed below, is fixedto the vacuum starwheel body assembly 450. Thus, the traveling hubassembly radial bearing outer race 652 is also fixed to the vacuumstarwheel body assembly 450.

As shown in FIGS. 21-26, the traveling hub assembly positioning keyassembly 580 includes a first wedge body 670, a second wedge body 672, aretainer body 674, and an actuator 676. The traveling hub assemblypositioning key assembly first wedge body 670 and traveling hub assemblypositioning key assembly second wedge body 672 are movably coupledtogether in a configuration wherein the combined wedge bodies 670, 672generally form a parallelepiped. That is, the combined wedge bodies 670,672 have two generally parallel upper/lower surfaces and two generallyparallel lateral surfaces. The interface between the traveling hubassembly positioning key assembly first wedge body 670 and traveling hubassembly positioning key assembly second wedge body 672 includes anumber of angled surfaces 680, 682. That is, the traveling hub assemblypositioning key assembly body angled surfaces 680, 682 are not parallelto the outer surfaces.

In an exemplary embodiment, the traveling hub assembly positioning keyassembly first wedge body 670 has a generally L-shaped cross-section andthe traveling hub assembly positioning key assembly second wedge body672 has a generally rectangular cross-section. The traveling hubassembly positioning key assembly second wedge body 672 is sized andshaped to correspond to the size and shape of the interior surface ofthe L-shaped traveling hub assembly positioning key assembly first wedgebody 670. In this configuration, the traveling hub assembly positioningkey assembly first wedge body 670 and traveling hub assembly positioningkey assembly second wedge body 672 have two surfaces that are directlycoupled to each other. As shown, at least one of these surfaces on eachbody are the traveling hub assembly positioning key assembly body angledsurfaces 680, 682. In this configuration, the traveling hub assemblypositioning key assembly 580 includes a very limited number of operativebodies 670, 672. As used herein, an “operative body” in a positioningkey means the bodies with an angled surface.

The traveling hub assembly positioning key assembly first wedge body 670also defines a threaded actuator bore 671. The traveling hub assemblypositioning key assembly second wedge body 672 further includes anoffset tab 673 defining an actuator passage 678 and a number of couplingcomponents, such as, but not limited to threaded bores 679. Thetraveling hub assembly positioning key assembly retainer body 674 alsodefines an actuator passage 686 with a retainer plenum 688. The retainerbody 674 also defines a number of fastener passages 690 that arestructured to, and do, align with the traveling hub assembly positioningkey assembly second wedge body threaded bores 679. The traveling hubassembly positioning key assembly actuator 676 includes a body 700 withan elongated threaded portion 702, a radially extending flange 704, anda tool interface 706 such as, but not limited to, a six-sided lug.

The traveling hub assembly positioning, key assembly 580 is, in oneembodiment, assembled as follows. That is, the order in which theelements are configured is not required to be as described below, solong as the final configuration is as described below. The traveling hubassembly positioning key assembly first wedge body 670 and traveling hubassembly positioning key assembly second wedge body 672 are positionedwith the traveling hub assembly positioning key assembly body angledsurfaces 680, 682 in contact with each other. The traveling hub assemblypositioning key assembly actuator 676 is passed through the travelinghub assembly positioning key assembly second wedge body 672 actuatorpassage 678 and is threaded into the traveling hub assembly positioningkey assembly first wedge body actuator bore 671. The traveling hubassembly positioning key assembly actuator tool interface 706 is passedthrough the traveling hub assembly positioning key assembly retainerbody actuator passage 686 so that the traveling hub assembly positioningkey assembly retainer body 674 abuts the traveling hub assemblypositioning key assembly second wedge body offset tab 673. In thisconfiguration, the traveling hub assembly positioning key assemblyretainer body 674 is coupled, directly coupled, or fixed to thetraveling hub assembly positioning key assembly second wedge body 672 byfasteners extending through the traveling hub assembly positioning keyassembly retainer body fastener passages 690 and into the traveling hubassembly positioning key assembly second, wedge body threaded bores 679.In this configuration, the traveling hub assembly positioning keyassembly actuator flange 704 is trapped in the traveling hub assemblypositioning key assembly retainer body retainer plenum 688. Thus, thetraveling hub assembly positioning key assembly 580 is a “unit assembly”as defined above.

Further, the traveling hub assembly positioning key assembly actuatortool interface 706 is exposed and is structured to be manipulated. Thatis, the traveling hub assembly positioning key assembly actuator toolinterface 706 is structured to be rotated. Rotation of the traveling hubassembly positioning key assembly actuator tool interface 706 causes thetraveling hub assembly positioning key assembly first wedge body 670 andtraveling hub assembly positioning key assembly second wedge body 672 tomove longitudinally relative to each other. Moreover, because thetraveling hub assembly positioning key assembly first wedge body 670 andtraveling hub assembly positioning key assembly second wedge body 672interface at the traveling hub assembly positioning key assembly bodyangled surfaces 680, 682, this motion causes the traveling hub assemblypositioning key assembly 580 to increase (or decrease, depending uponthe direction the traveling hub assembly positioning key assemblyactuator 676 is rotated) in the cross-sectional area. That is, thetraveling hub assembly positioning key assembly 580 moves between twoconfigurations; a smaller, first configuration, wherein thecross-sectional area of the traveling hub assembly positioning keyassembly 580 is relatively smaller (which, as used herein, meansrelative to the second configuration of the positioning key assembly),and a larger, second configuration, wherein the cross-sectional area ofthe traveling hub assembly positioning key assembly 580 is relativelylarger (which, as used herein, means relative to the first configurationof the positioning key assembly). As described below, the positioningkey assembly 580 is structured to align the vacuum starwheel bodyassembly 450/traveler assembly collar 620 with the rotating shaftassembly rotating shaft 416 axis of rotation. Thus, these configurationsare alternately described as the positioning key assembly 580 beingstructured to move between a smaller, first configuration, wherein thepositioning key assembly 580 does not align the vacuum starwheel bodyassembly 450/traveler assembly collar 620 with the rotating shaftassembly rotating shaft 416 axis of rotation, and, a larger, secondconfiguration, wherein the positioning key assembly 580 aligns thevacuum starwheel body assembly 450/traveler assembly collar 620 with therotating shaft assembly rotating shaft 416 axis of rotation. It is notedthat the outer surfaces of the traveling hub assembly positioning keyassembly 580 remain generally parallel as the traveling hub assemblypositioning key assembly first wedge body 670 and traveling hub assemblypositioning key assembly second wedge body 672 move relative to eachother.

The quick-change vacuum starwheel assembly 400 is, in one embodiment,assembled as follows. That is, the order in which the elements areconfigured is not required to be as described below, so long as thefinal configuration is as described below. It is understood that thequick-change vacuum starwheel assembly 400 is coupled to a processingstation 20 with the rotating shaft assembly housing assembly 412coupled, directly coupled, or fixed to the frame assembly 12. Therotating shaft assembly rotating shaft 416 extends through the rotatingshaft assembly housing assembly 412. As noted above, the rotating shaftassembly rotating shaft 416 is operatively coupled to the drive assembly2000 and is structured to, and does, rotate. The quick-change vacuumstarwheel height adjustment assembly base assembly fixed base member 562is fixed to the rotating shaft assembly housing assembly 412. The firstinner guiderail 352A and the second inner guiderail 353A are coupled,directly coupled, or fixed to the quick-change vacuum starwheel heightadjustment assembly base assembly fixed base member 562 by a singleretained coupling 664.

The rotating shaft assembly housing assembly 412, the rotating shaftassembly rotating shaft 416, the quick-change vacuum starwheel heightadjustment assembly base assembly fixed base member 562, the first innerguiderail 352A and the second inner guiderail 353A are structured toremain in the same position relative to the frame assembly 12. That is,other than rotating about the axis of rotation, the rotating shaftassembly rotating shaft 416 does not move relative to the frame assembly12.

The quick-change vacuum starwheel height adjustment assembly baseassembly elongated support members 566 are movably coupled to thequick-change vacuum starwheel height adjustment assembly base assemblyfixed base member 562. That is, the quick-change vacuum starwheel heightadjustment assembly base assembly elongated support members 566 areslidably disposed in the quick-change vacuum starwheel height adjustmentassembly base assembly fixed base member support member passages 563.The quick-change vacuum starwheel height adjustment assembly baseassembly movable base member 564 is fixed to the quick-change vacuumstarwheel height adjustment assembly base assembly elongated supportmembers 566 and move therewith. The vacuum assembly telescoping vacuumconduit 484 is coupled to the quick-change vacuum starwheel heightadjustment assembly base assembly movable base member 564 and extendsand retracts telescopically therewith.

The vacuum assembly vacuum housing assembly 486 is also coupled,directly coupled, or fixed to the quick-change vacuum starwheel heightadjustment assembly base assembly movable base member 564 with therotating shaft assembly rotating shaft 416 extending through the vacuumassembly vacuum housing assembly movable mounting portion body rotatingshaft passage 518. The traveling hub assembly radial bearing 578 iscoupled, directly coupled, or fixed to the vacuum assembly vacuumhousing assembly 486 and extends about the rotating shaft assemblyrotating shaft 416. That is, the traveling hub assembly radial bearing578 separates the vacuum assembly vacuum housing assembly 486 and therotating shaft assembly rotating shaft 416.

The traveler assembly 576 is assembled with the traveler assemblytraveler mounting 630 fixed to the traveler assembly collar 620. Asnoted above, in the embodiment shown, wherein there are four starwheelbody assembly body segments 452, the traveler assembly traveler mounting630 includes four groups of a traveler assembly traveler mounting bodyretained coupling 636 and two traveler assembly traveler mounting bodylugs 638, 640. The traveler assembly traveler mounting 630 is fixed tothe traveler assembly collar 620. As noted above, the traveler assemblytraveler mounting 630 and the traveler assembly collar 620 are, in oneembodiment, coupled by fasteners, or, in another embodiment, are aunitary body. Thus, the traveler assembly traveler mounting 630 isstructured to, and does, rotate with the traveler assembly collar 620.

The traveling hub assembly 570 is coupled and, as discussed below, fixedto the rotating shaft assembly rotating shaft distal end 422. That is,as noted above, the traveling hub assembly radial bearings 578 aredisposed about the rotating shaft assembly rotating shaft 416. Thetraveler assembly collar 620 is also disposed about the rotating shaftassembly rotating shaft 416 and the traveling hub assembly radialbearings 578 are coupled, directly coupled, or fixed to the travelerassembly collar 620. That is, the traveler assembly collar body retainedrelease coupling 625 is disposed in the first position and the travelerassembly collar body 622 is moved over the rotating shaft assemblyrotating shaft 416 until the traveler assembly collar body 622 isdisposed immediately adjacent to the traveling hub assembly radial,bearing 578. The traveler assembly collar body 622 and the traveling hubassembly radial bearing 578 are fixed together. The traveler assemblycollar body retained release coupling 625 is moved to the secondposition wherein the traveler assembly collar body 622 is fixed to therotating shaft assembly rotating shaft 416. The traveler assembly collarbody 622 is oriented so that the four groups of a traveler assemblytraveler mounting body retained coupling 636 and two traveler assemblytraveler mounting body lugs 638, 640 are disposed on the front surfaceof traveler assembly traveler mounting body 632, i.e., the surfacedisposed away from the frame assembly 12.

The traveling, hub assembly actuator 574 and the traveler bracket 610are operatively coupled with the traveling hub assembly actuator 574disposed through, and threadably coupled to, the traveler assemblytraveler bracket central passage 614. The traveling hub assemblyactuator 574 is disposed in the traveler hub mounting central cavity 426with the traveler bracket body arms 616, 617 each disposed in separatetraveler hub mounting slots 428, 430. Further, the traveling hubassembly actuator body second end rotatable mounting 602 is rotatablycoupled to the traveler hub mounting central cavity rotational couplingcavity 427. The traveler bracket 610 is coupled, directly coupled, orfixed to the traveler assembly collar 620 by fasteners 619 extendingthrough each of the traveler bracket body arm passages 618 and into thethreaded bores on the front axial surface of the traveler assemblycollar body 622. In this configuration, the traveler bracket 610 isfixed to the traveler assembly collar body 622.

The traveling hub assembly base 572 is fixed to the rotating shaftassembly rotating shaft body distal end 422 with the traveling hubassembly actuator body first end 594, the hex-head lug 598, extendingthrough the traveling hub assembly base body central opening. That is,fasteners 582 extending through the traveling hub assembly base body 581are coupled to the threaded bores disposed on the axial surface of therotating shaft assembly rotating shaft body distal end 422. In thisconfiguration, the traveling hub assembly base 572 is fixed to therotating shaft assembly rotating shaft body 418

Further, the traveling hub assembly positioning key assembly 580, andmore specifically the traveling hub assembly positioning key assemblyfirst wedge body 670, is fixed to the traveler assembly collar bodypositioning key mounting 626. In this configuration, the traveling hubassembly positioning key assembly 580 is, as used herein, a retainedcoupling and/or a retained release coupling. Moreover, the positioningkey assembly 580 is one of the quick-change height adjustment assemblyretained release couplings 552. In this configuration, the traveling hubassembly positioning key assembly 580 is disposed between the rotatingshaft assembly positioning key mounting 432 and the traveler assemblycollar body positioning key mounting 626. Stated alternately, when therotating shaft assembly positioning key mounting 432 and the travelerassembly collar body positioning key mounting 626 are aligned anddisposed generally opposite, each other, the rotating shaft assemblypositioning key mounting 432 and the traveler assembly collar bodypositioning key mounting 626 define, as used herein, a “quick-changevacuum starwheel assembly positioning key cavity” 583. The traveling hubassembly positioning key assembly 580 is structured to correspond to thequick-change vacuum starwheel assembly positioning, key cavity 583. Thatis, in the first configuration, the traveling hub assembly positioningkey assembly 580 loosely fits within the quick-change vacuum starwheelassembly positioning key cavity 583. When the traveling hub assemblypositioning key assembly 580 is in the second configuration, i.e., theconfiguration with the greater cross-sectional area, the traveling hubassembly positioning key assembly 580 moves the traveler assembly collar620 into alignment with the rotating shaft assembly rotating shaft 416axis of rotation. That is, as the traveling hub assembly positioning keyassembly 580 moves into the second configuration, i.e., as thecross-sectional area of the quick-change vacuum starwheel assemblypositioning key assembly 580 increases, the quick-change vacuumstarwheel assembly positioning key assembly 580 operatively engages therotating shaft assembly rotating shaft 416 and the traveler assemblycollar 620 and moves these elements into alignment with each other. Asused in this context, “into alignment” means that the axis of rotationfor the rotating shaft assembly rotating shaft 416 and the travelerassembly collar 620 are substantially aligned, i.e., coextensive witheach other.

The vacuum starwheel body assembly body segments 452 are coupled,directly coupled, or fixed to the traveler assembly traveler mounting630. That is, each vacuum starwheel body assembly body segment 452 iscoupled to the traveler assembly traveler mounting 630 by coupling thestarwheel body assembly body segment axial mounting portion passages466, 468, 469 with their associated traveler assembly traveler mountingbody retained coupling 636 and alignment lugs 638, 640. It is noted thateach starwheel body assembly body segment 452 is coupled to the travelerassembly traveler mounting 630 by a single retained traveler assemblytraveler mounting body retained coupling 636.

In this configuration, the starwheel body assembly body sealing surface474 sealingly engages the vacuum seal assembly body 542. Thus, thestarwheel body cavity 472 is substantially sealed and resists the flowof air through openings other than the starwheel body assembly bodysegment peripheral pocket passages 470. Further, in this configuration,the vacuum assembly 480 is in fluid communication with the non-baffledstarwheel body assembly body segment peripheral pocket passages 470.

Further, as noted above, the first inner guiderail 352A and second innerguiderail 353A are each coupled, directly coupled, or fixed to the innerguiderail mounting block 660 by a single retained coupling 664. Theinner guiderail mounting block 660 is coupled, directly coupled, orfixed to the quick-change vacuum starwheel height adjustment assemblybase assembly fixed base member 562. The first outer guiderail 354A andthe second outer guiderail 355A are each coupled, directly coupled, orfixed to the outer guiderail mounting block 662 by a single retainedcoupling 664. The outer guiderail mounting block 662 is coupled,directly coupled, or fixed to the quick-change vacuum starwheel heightadjustment assembly base assembly movable base member 564 and movestherewith. It is understood that the quick-change vacuum starwheelassembly guide assembly guiderails 350A are positioned and oriented sothat the guide surfaces 360A are disposed a guiding distance from theassociated starwheel 32. That is, the inner and outer guiderail mountingblocks 660, 662 include an orientation lug (not shown) that isstructured to be, and is, coupled to an orientation notch (not shown) onthe inner guiderail 352 and/or the outer guiderail 354. The orientinglug and, the orientation notch are structured to, and do, position theguiderail guide surfaces 360 at a guiding distance relative to a canbody 1.

In this configuration, the rotating shaft assembly housing assembly 412,the quick-change vacuum starwheel height adjustment assembly baseassembly fixed base member 562, the first inner guiderail 352A and thesecond inner guiderail 353A are structured to remain in the sameposition relative to the frame assembly 12. Further, with the travelinghub assembly positioning key assembly 580 in the second configurationand the traveler assembly collar body retained release coupling 625 inthe second configuration, the traveling hub assembly 570 and the vacuumstarwheel body assembly 450 are fixed to the rotating shaft assemblyrotating shaft 416 and rotates therewith. Further, the vacuum assembly480 is in fluid communication with the starwheel body cavity 472. Thisis the operational configuration for the quick-change vacuum starwheelassembly 400.

To adjust the quick-change vacuum starwheel assembly 400 for can bodieshaving different heights, only two couplings need to be actuated; thetraveling hub assembly positioning key assembly 580 and the travelerassembly collar body retained release coupling 625. That is, when thetraveling hub assembly positioning key assembly 580 is moved to thefirst configuration, the bias created by the positioning key assembly580 being in the second configuration, is reduced. When the travelerassembly collar body retained release coupling 625 is in the firstposition, the traveler assembly collar 620 is no longer fixed to therotating shaft assembly rotating shaft 416. Thus, the traveler assemblycollar 620, as well as all elements fixed thereto, are free to movelongitudinally along the rotating shaft assembly rotating shaft 416.Thus, the disclosed configuration is a quick-change height adjustmentassembly 550 as defined above.

The elements fixed to the traveler assembly collar 620 include: thetraveler assembly traveler mounting 630, the vacuum starwheel bodyassembly 450 (which is fixed to the traveler assembly traveler mounting630), the traveling hub assembly radial bearing 578 (which is fixed tothe traveler assembly collar 620 and the vacuum assembly 480), thevacuum assembly 480, the quick-change vacuum starwheel height adjustmentassembly base assembly movable base member 564 (which is fixed to thevacuum assembly 480), the quick-change vacuum starwheel heightadjustment assembly base assembly elongated support members 566 (whichare fixed to the quick-change vacuum starwheel height adjustmentassembly base assembly movable base member 564), and the outer guiderailmounting block 662 with the first outer guiderail 354A and the secondouter guiderail 355A (which are fixed to the quick-change vacuumstarwheel height adjustment assembly base assembly movable base member564). It is understood that the vacuum assembly telescoping vacuumconduit 484 allows the other vacuum assembly 480 components to moverelative to the vacuum generator 482.

Movement of the traveler assembly collar 620, and elements fixedthereto, is accomplished by rotating the traveling hub assembly actuator574. In an exemplary embodiment, a tool (not shown) is operativelycoupled to the traveling hub assembly actuator body first end hex-headlug 598. The traveling hub assembly actuator 574 is then rotated. As thetraveling hub assembly actuator body first end 594 is in a fixedlocation relative to the rotating shaft assembly rotating shaft distalend 422, and because the traveling hub assembly actuator 574 isthreadably coupled to the traveler assembly traveler bracket centralpassage 614, rotation of the traveling hub assembly actuator 574 causesthe traveler bracket 610 to move along the rotating shaft assemblyrotating shaft 416 axis of rotation. Because the traveler bracket 610 isfixed to the traveler assembly collar 620, the traveler assembly collar620 and elements fixed thereto, also move along the rotating shaftassembly rotating shaft 416 axis of rotation. Stated alternately,actuation of the traveling hub assembly actuator 574 moves the vacuumstarwheel body assembly 450 and the vacuum assembly 480 between a firstlongitudinal position on the rotating shaft assembly rotating shaft 416and a second longitudinal position on the rotating shaft assemblyrotating shaft 416. Stated in a further alternate form, the quick-changevacuum starwheel height adjustment assembly 550 is structured to be, andis, actuated after only the two retained release couplings 552 areconfigured in a first configuration. Thus, the position of the vacuumstarwheel body assembly 450 is adjusted to accommodate can bodies of adifferent height. Further, the disclosed quick-change vacuum starwheelheight adjustment assembly 550 is structured to, and does, allow thestarwheel 32 to move between two configurations, a first configurationfor a can body 1 of a first height and a second configuration for a canbody 1 of a second height, without the use of a spacer. Further, thedisclosed quick-change vacuum starwheel height adjustment assembly 550is structured to, and does, allow the vacuum starwheel 32 to movebetween two configurations, a first configuration for a can body 1 of afirst height and a second configuration for a can body 1 of a secondheight, without altering the configuration of the vacuum starwheel 32.That is, the quick-change vacuum starwheel height adjustment assembly550 is structured to, and does, move relative to a fixed location, suchas, but not limited to, the frame assembly 12, but the vacuum starwheelbody assembly 450 does not change configuration.

The quick-change vacuum starwheel mounting assembly 800 is structured toallow a first vacuum starwheel 32 to be swapped for a second vacuumstarwheel 32 having different characteristics. Generally, the differentcharacteristics will be pockets 34 having a different radius, but vacuumstarwheels 32 are swapped out for other reasons as well. It isunderstood that to swap vacuum starwheels 32 the first vacuum starwheel32 and the components associated with a starwheel of that size must beremoved and replaced. Moreover, as noted above, a “quick-change vacuumstarwheel mounting assembly” 800 means a mounting assembly structured tocouple, directly couple, or fix the separable vacuum starwheelcomponents to a rotating shaft via one of a limited number of couplings,a significantly limited number of couplings, a very limited number ofcouplings, or an exceedingly limited number of couplings. The “separablevacuum starwheel components,” as used herein, are the individualelements of vacuum starwheel 32 (also identified as the vacuum starwheelbody assembly 450) which are identified herein as the separate vacuumstarwheel body assembly body segments 452 as well as the quick-changevacuum starwheel assembly guide assembly 300A associated with a vacuumstarwheel 32 of a specific size which are identified herein as the firstinner guiderail 352A, the second inner guiderail 353A, the first outerguiderail 354A, and the second outer guiderail 355A. These elements havebeen described above.

As shown in FIG. 11, the quick-change vacuum starwheel mounting assembly800 includes a number of separable vacuum starwheel components 802(identified above and collectively by reference number 810) and one of alimited number of retained couplings 804, a significantly limited numberof retained couplings 804, a very limited number of retained couplings804, or an exceedingly limited number of retained couplings 804(discussed above and collectively by reference number 804) as well asthe construct(s) to which the retained couplings 804 are coupled(discussed below). Each quick-change vacuum starwheel mounting assemblyseparable vacuum starwheel component 802 (hereinafter, “separable vacuumstarwheel component(s)” 802) is coupled, directly coupled, or fixed tothe rotating shaft assembly housing assembly 412 (or any fixed locationon a processing station 20 or the transfer assembly 30) by one of asignificantly limited number of retained couplings 804, a very limitednumber of retained couplings 804 or an exceedingly limited number ofretained couplings 804.

In an exemplary embodiment, and as discussed above, the vacuum starwheelbody assembly 450 includes a number of vacuum starwheel body assemblybody segments 452. Each vacuum starwheel body assembly body segment 452is removed when exchanging a vacuum starwheel body assembly 450, so eachvacuum starwheel body assembly body segment 452 is also a “separablevacuum starwheel component” 802. Each vacuum starwheel body assemblybody segment 452 is structured to be, and is, coupled to the travelerassembly traveler mounting 630. As discussed above, each vacuumstarwheel body assembly body segment 452 includes a group of a single,or an exceedingly limited number of, retained coupling passage 466, afirst lug passage 468, and a second lug passage 469 disposed along anarc. Thus, for each vacuum starwheel body assembly body segment 452 tobe coupled to the traveler assembly traveler mounting 630, the travelerassembly traveler mounting 630 includes a group including a travelerassembly traveler mounting body retained coupling 636, a first alignmentlug 638 and a second alignment lug 640 disposed along an arccorresponding to the starwheel, body assembly body segment axialmounting portion passages 466, 468, 469. Thus, each vacuum starwheelbody assembly body segment 452 is coupled to the traveler assemblytraveler mounting 630 by an exceedingly limited number of travelerassembly traveler mounting body retained couplings 636.

As defined above, the quick-change vacuum starwheel assembly guiderails350 are included as “separable vacuum starwheel components 802.” Thatis, each quick-change vacuum starwheel assembly guiderail 350 has aguide surface 360A that is structured to be, and is, disposed a guidingdistance from a vacuum starwheel body assembly 450 of a specific size.Thus, when the vacuum starwheel body assembly 450 is exchanged, thequick-change vacuum starwheel assembly guiderails 350 are exchanged aswell. As discussed above, the quick-change vacuum starwheel assemblyguide assembly 300A includes a number of guiderails 350A. Each guiderail350A is coupled (via a number of other elements) to the rotating shaftassembly housing assembly 412. That is, the quick-change vacuumstarwheel assembly guiderails 350 include an inner guiderail mountingblock 660 and an outer guiderail mounting block 662. The inner guiderailmounting block 660 and the outer guiderail mounting block 662 arecoupled (via a number of other elements) to the rotating shaft assemblyhousing assembly 412. Each guiderail 350A is coupled to one of theguiderail mounting blocks 660, 662 by an exceedingly limited number ofretained couplings 664.

Generally, each processing station 20 is structured to partially formthe can body 1 so as to reduce the cross-sectional area of the can bodyfirst end 6. The processing stations 20 include some elements that areunique to a single processing station 20, such as, but not limited to, aspecific die. Other elements of the processing stations 20 are common toall, or most, of the processing stations 20. The following discussion isrelated to the common elements and, as such, the discussion is directedto a single generic processing (forming) station 20 (hereinafter, a“forming station” 20′). It is understood, however, that any processingstation 20 can include the elements discussed below.

As shown in FIG. 27, each forming station 20′ includes a quick-changeassembly 900, an inboard turret assembly 1000 and an outboard turretassembly 1200. Further, as is known, elements of the inboard turretassembly 1000 and the outboard turret assembly 1200 are generallyseparated by a gap 1001 and the can bodies 1 move in between the inboardturret assembly 1000 and the outboard turret assembly 1200, i.e., in thegap 1001. The quick-change assembly 900 is structured to, and does,couple selected elements of the inboard turret assembly 1000 and theoutboard turret assembly 1200 to at least one of the frame assembly, theinboard turret assembly or the outboard turret assembly by one of alimited number of couplings, a significantly limited number ofcouplings, a very limited number of couplings, or an exceedingly limitednumber of couplings.

That is, the forming station quick-change assembly 900 is structured to,and does, allow for rapid replacement of elements in a forming station20′. As used herein, a “forming station quick-change assembly 900”includes, for a number of elements (or sub-components) coupled to theforming station 20′, couplings having one of a limited number ofretained couplings, a significantly limited number of retainedcouplings, a very limited number of retained couplings, an exceedinglylimited number of retained couplings, and/or, a limited number ofretained release couplings, a significantly limited number of releasecouplings, a very limited number of retained release couplings, and/oran exceedingly limited number of retained release couplings. Theelements of the forming station quick-change assembly 900 are discussedbelow.

Generally, the inboard turret assembly 1000 includes a frame assembly 12(which is part of the larger frame assembly 12, discussed above), anumber of fixed elements 1002 and a number of movable elements 1004. Theinboard turret assembly fixed elements 1002 are coupled, directlycoupled, or fixed to the frame assembly 12 and generally do not moverelative thereto. The fixed elements include a cam ring 1010. Theinboard turret assembly movable elements 1004 include a vacuum starwheel32 (as discussed above) and an elongated process shaft assembly 1020that is rotatably coupled to the frame assembly 12. The vacuum starwheel32 is generally disposed at the gap 1001. Other known elements of theinboard turret assembly 1000 are known but are not relevant to thisdiscussion. The inboard turret assembly cam ring 1010 (as well as theoutboard turret assembly cam ring) is generally circular with an offsetportion that is offset toward the gap 1001.

The inboard turret assembly process shaft assembly 1020 (hereinafter,the “process shaft assembly 1020”) includes an elongated shaft 1022(also identified herein as “process shaft assembly body” 1022). Theprocess shaft assembly shaft 1022 is, in one embodiment, a unitary body(not shown), or, in another embodiment an assembly of shaft segments1024A, 1024B, etc. It is understood that the shaft segments 1024A, 1024Bare fixed together and rotate as a single body 1024. The process shaftassembly shaft 1022 is operatively coupled to the drive assembly 2000and is structured to, and does, rotate relative to the frame assembly12. As discussed below, the outboard turret assembly 1200 also includesa number of rotating elements, i.e., the outboard turret assembly upperportion pusher assemblies 1260, discussed below. The outboard turretassembly 1200 rotating elements are coupled, directly coupled, or fixedto the process shaft assembly 1020 and rotate therewith.

In an exemplary embodiment, the process shaft assembly 1020 includes aknockout ram mounting 1030, a plurality of knockout ram assemblies 1040,a number of die assemblies 1060, a die assembly support 1080, and astarwheel assembly 1090. The starwheel assembly 1090 is not a vacuumstarwheel 32 as discussed above, but rather a guide starwheel 1092 thatincludes a generally planar, generally toroid body assembly 1094including a number of segments 1096 (two shown, each extending over anarc of about 180°). As is known, the radial surface of the guidestarwheel body assembly 1094 defines a number of pockets 1100 sized togenerally correspond to the radius of a can body 1. It is understoodthat for can bodies having different radii, different guide starwheels1092 are needed.

The forming station quick-change assembly 900 includes a starwheelmounting 902 and a number of starwheel retained couplings 904. Theforming station quick-change assembly starwheel mounting 902 includes atoroid body 906 that is coupled, directly coupled, or fixed to, theprocess shaft assembly shaft 1022. The starwheel retained couplings 904are coupled to the exposed (away from the frame assembly 12) axialsurface of the forming station quick-change assembly starwheel mounting902. In an exemplary embodiment, there is one of a very limited numberof starwheel retained couplings 904 or apt exceedingly limited number ofstarwheel retained couplings 904 associated with each guide starwheelbody assembly segment 1096. It is understood that each guide starwheelbody assembly segment 1096 includes a number of passages 1098 disposedin a pattern corresponding to the pattern of starwheel retainedcouplings 904. In an exemplary embodiment, wherein each guide starwheelbody assembly segment 1096 includes an exceedingly limited number ofpassages 1098, there are also a number of lug passages (which are notcouplings as used herein) (not shown). In this embodiment, not shown,the forming station quick-change assembly starwheel mounting 902includes a number of lugs (not shown) on the exposed (away from theframe assembly 12) axial surface of the forming station quick-changeassembly starwheel mounting 902. Thus, each guide starwheel bodyassembly segment 1096 is coupled to the forming station quick-changeassembly starwheel mounting 902. Moreover, when the necker machine 10needs to be changed to accommodate can bodies with a different radii,the guide starwheel body assembly 1094 is swapped using the formingstation quick-change assembly 900 elements discussed herein. This solvesthe problem stated above.

The outboard turret assembly 1200 includes an upper portion 1202 and alower portion 1204. The outboard turret assembly lower portion 1204includes a base 1206 that is disposed in a fixed location relative tothe inboard turret assembly 1000. That is, the outboard turret assemblylower portion 1204 is fixed to the frame assembly 12, or, fixed to asubstrate (not numbered). In this configuration, the outboard turretassembly lower portion 1204 is structured to not move, and does notmove, relative to the inboard turret assembly 1000. The outboard turretassembly lower portion base 1206 includes a number of guide elementswhich are, as shown, elongated, substantially straight rails 1208.

The outboard turret assembly upper portion 1202 includes a base assembly1210, a support assembly 1212, a cam ring 1214, and pusher assembly1260. The outboard turret assembly upper portion base assembly 1210, theoutboard turret assembly upper portion support assembly 1212, and theoutboard turret assembly upper portion cam ring 1214 are, in anexemplary embodiment, coupled, directly coupled, or fixed to each otherand do not move relative to each other. The outboard turret assemblyupper portion base assembly 1210 includes a housing 1220 including anumber of guide followers which are, as shown, rail passages 1222.

The outboard turret assembly upper portion 1202 is movably coupled tothe outboard turret assembly lower portion base 1206. That is, theoutboard turret assembly upper portion base assembly housing railpassages 1222 are disposed over the outboard turret assembly lowerportion base rails 1208. Further, as noted above, the process shaftassembly shaft 1022 extends into, or through, the outboard turretassembly upper portion pusher assembly 1260 and is movably coupledthereto. Thus, the outboard turret assembly upper portion pusherassembly 1260 is structured to, and does, rotate with the process shaftassembly shaft 1022.

In this configuration, the outboard turret assembly upper portion 1202is structured to, and does, move axially, i.e., longitudinally, over theprocess shaft assembly shaft 1022. That is, the outboard turret assemblyupper portion 1202 is structured to, and does, move between a firstposition, wherein the outboard turret assembly upper portion 1202 isdisposed closer to the inboard turret assembly 1000 (closer being arelative term that is relative to the second position), and a secondposition, wherein the outboard turret assembly upper portion 1202 isdisposed further from the inboard turret assembly 1000 (further being arelative term that is relative to the first position). It is understoodthat this motion allows the forming station 20′ to be configured toprocess can bodies 1 of different heights. That is, for relatively shortcan bodies, the outboard turret assembly upper portion 1202 is in thefirst position and for relatively longer can bodies, the outboard turretassembly upper portion 1202 is in the second position.

The forming station quick-change assembly 900 includes a “single pointmovement assembly” 920 that is structured to, and does, move theoutboard turret assembly upper portion 1202 between the first and secondpositions. As used herein, a “single point movement assembly” 920 is aconstruct having a single actuator for a movement assembly, or, a singleactuator for a movement assembly and a single actuator for a lockingassembly. The single point movement assembly 920 is disposed at theoutboard turret assembly 1200. In an exemplary embodiment, the singlepoint movement assembly 920 includes a jackscrew (not shown) having arotary actuator 922, a jackscrew retainer (not shown), a lockingassembly (generally not shown) with a single locking assembly actuator924. The jackscrew retainer is a threaded collar that is structured to,and does, operatively engage the jackscrew threads. The jackscrewretainer is coupled, directly coupled, or fixed to the outboard turretassembly upper portion 1202. The jackscrew is rotatably coupled to theoutboard turret assembly lower portion base 1206. As is known, thelongitudinal axis (axis of rotation) of the jackscrew extends generallyparallel to the outboard turret assembly lower portion base rails 1208.In this configuration, actuation of the single point movement assemblyrotary actuator 922 causes the outboard turret assembly upper portion1202 to move between the first and second positions. This solves theproblem noted above. The single point movement assembly single lockingassembly actuator 924 is coupled to a cam assembly (not shown). The camassembly is coupled, directly coupled, or fixed to the outboard turretassembly upper portion 1202. The can is structured to, and does, movebetween an unlocked, first configuration, wherein the cam does notengage a portion of the outboard turret assembly lower portion 1204 andthe outboard turret assembly upper portion 1202 is free to move relativeto the outboard turret assembly lower portion 1204, and, a locked,second position, wherein the cam engages a portion of the outboardturret assembly lower portion 1204 and the outboard turret assemblyupper portion 1202 is not free to move relative to the outboard turretassembly lower portion 1204.

The single point movement assembly 920, and in an exemplary embodiment,the jackscrew/jackscrew retainer as well as the cam assembly, are each aretained coupling assembly and/or a retained release coupling assembly.Moreover, the single point movement assembly 920 includes a limitednumber of retained couplings. Thus, the outboard turret assembly upperportion 1202 is structured to be moved between the first position andthe second position via the actuation of a limited number of retainedcouplings or retained release couplings.

The outboard turret assembly 1200, and in an exemplary embodiment theoutboard turret assembly upper portion 1202, further includes a pusherram block 1250 and a number of pusher assemblies 1260. In an exemplaryembodiment, the pusher ram block 1250 includes a toroid body that iscoupled, directly coupled, or fixed to the process shaft assembly shaft1022 and rotates therewith. As is known, each pusher assembly 1260 isstructured to temporarily support a can body 1 and move the can bodytoward an associated die assembly 1060. For the can body 1 supported bythe pusher assemblies 1260 to properly engage the associated dieassemblies 1060, the pusher assemblies 1260 must be aligned with theassociated die assemblies 1060. This is accomplished using a positioningkey.

As shown in FIG. 28, the outboard turret assembly 1200 includes apositioning key assembly 1280. The outboard turret assembly positioningkey assembly 1280 is substantially similar to the traveling hub assemblypositioning key assembly 580 discussed above. As the outboard turretassembly positioning key assembly 1280 is substantially similar to thetraveling hub assembly positioning key assembly 580, details of theoutboard turret assembly positioning key assembly 1280 are not discussedherein but it is understood that similar elements exist and areidentified by the collective adjective “outboard turret assemblypositioning key assembly [X] ” and the reference numbers for thoseelements are +700 relative to the elements of the traveling hub assemblypositioning key assembly 580, For example, the traveling hub assemblypositioning key assembly 580 includes a first wedge body 670; thus, theoutboard turret assembly positioning key assembly 1280 includes a firstwedge body 1370.

As shown in FIG. 29, the outboard turret assembly pusher ram block 1250defines a positioning key mounting 1252 and the process shaft assemblyshaft 1022 defines a corresponding, positioning key mounting 1254. Thatis, the outboard turret assembly pusher ram block 1250 is positioned onthe process shaft assembly shaft 1022 with the outboard turret assemblypusher ram block positioning key mounting 1252 disposed opposite theprocess shaft assembly shaft, positioning key mounting 1254 whereby thetwo positioning key mountings create a forming station shaft assemblyquick-change assembly positioning key assembly cavity 1256. The outboardturret assembly positioning key 1280 is disposed in the forming stationshaft assembly quick-change assembly positioning key assembly cavity1256. In a manner substantially similar to the traveling hub assemblypositioning key assembly 580 described above, the outboard turretassembly positioning key 1280 moves between a first configuration,wherein the cross-sectional area of the forming station shaft assemblyquick-change assembly positioning key assembly is relatively smaller andwherein the outboard turret assembly pusher ram block 1250 is notaligned with the process shaft assembly process shaft 1022, and, asecond configuration, wherein the cross-sectional area of the formingstation shaft assembly quick-change assembly positioning key assembly1280 is relatively larger and wherein the outboard turret assemblypusher ram block 1250 is aligned with the process shaft assembly processshaft 1021. Thus, the outboard turret assembly positioning key 1280 isstructured to, and does, move the pusher assemblies 1260 into alignmentwith the associated die assemblies 1060.

As shown in FIG. 27, the outboard turret assembly pusher ram block 1250further includes a number of pusher assembly linear bearings 1258. Asshown, the outboard turret assembly pusher ram block pusher assemblylinear bearings 1258 (hereinafter “pusher assembly linear bearings1258”) extend substantially parallel to the axis of rotation of theprocess shaft assembly shaft 1022. The pusher assembly linear bearings1258 are discussed further below.

As shown in FIGS. 30-34, the pusher assemblies 1260 are substantiallysimilar to each other and only one is described herein. As shown in FIG.28, the pusher assembly 1260 includes a housing 1400, a quick-releasemounting assembly 1410, and a pusher pad 1480. The pusher assemblyhousing 1400 includes a body 1402 defining a cavity 1404 and supportingtwo adjacent cam followers 1406, 1408. The pusher assembly housing 1400is movably coupled to the outboard turret assembly pusher ram block 1250and rotates therewith. More specifically, the pusher assembly housing1400 defines a bearing passage 1409. The pusher assembly housing 1400 ismovably coupled to the outboard turret assembly pusher ram block 1250with a pusher assembly linear bearing 1258 disposed in the pusherassembly housing bearing passage 1409. Further, the pusher assemblyhousing cam followers 1406, 1408 are operatively coupled to the outboardturret assembly upper portion cam ring 1214. Thus, as the outboardturret assembly pusher ram block 1250 rotates, each pusher assemblyhousing 1400 is structured to, and does, move between a retracted, firstposition, wherein the pusher assembly housing 1400 is closer to theoutboard turret assembly lower portion 1204, and, an extended, secondposition, wherein the pusher assembly housing 1400 is closer to theinboard turret assembly 1000.

It is understood that each pusher assembly pusher pad 1480 correspondsto, i.e., is structured to support, a can body 1 with a specific radius.Thus, when the necker machine 10 needs to process a can body 1 of adifferent radius, the pusher assembly pusher pads 1480 must beexchanged. The quick-release mounting assembly 1410, which is alsoidentified herein as an element of the forming station quick-changeassembly 900, is structured to allow the pusher assembly pusher pads1480 to be exchanged while using a very limited, or in an exemplaryembodiment, an exceedingly limited, number of retained couplings.

That is, as described below, each quick-release mounting assembly 1410is a retained release coupling assembly. Each quick-release mountingassembly 1410 includes a base 1412, a number of balls 1414 (one shown),a ball lock sleeve 1416, a ball retainer 1418 and a number of biasingdevices 1420. The quick-release mounting assembly biasing devices 1420are, in an exemplary embodiment, springs 1422. As shown, thequick-release mounting assembly base 1412, ball lock sleeve 1416, and aball retainer 1418 are generally cylindrical and torpid bodies 1413,1415, 1419, respectively. In an exemplary embodiment, the ball retainer1418 includes an outer sleeve. The pusher assembly quick-releasemounting assembly base 1412 includes a generally toroid body 1413,including an outer surface coupling 1421 such as, but not limited tothreads. It is understood that the pusher assembly housing body cavity1404 has a corresponding coupling. Thus, the pusher assemblyquick-release mounting assembly base 1412 is structured to be, and is,coupled, directly coupled, or fixed to the pusher assembly housing 1400.Each pusher assembly quick-release mounting assembly ball lock sleeve1416 includes a generally toroid body 1417 with a first end 1430, amedial portion 1432, and a second end 1434. The pusher assemblyquick-release mounting assembly ball lock sleeve body first end 1430includes a tapered portion 1431. The pusher assembly quick-releasemounting assembly ball lock sleeve body medial portion 1432 includes aninwardly extending radial lug 1436. The pusher assembly quick-releasemounting assembly ball retainer 1418 includes a generally toroid body1419 with a sleeve body lug slot 1450.

Each pusher assembly quick-release mounting assembly base 1412 iscoupled to the pusher assembly housing 1400 with the pusher assemblyquick-release mounting assembly base body 1413 substantially disposedwithin an associated pusher assembly housing mounting cavity 1404. Eachpusher assembly quick-release mounting assembly ball lock sleeve body1417 is movably disposed within an associated pusher assembly housingmounting cavity 1404 with the pusher assembly quick-release mountingassembly ball lock sleeve body first end 1430 disposed adjacent anassociated pusher assembly quick-release mounting assembly base 1412.The pusher assembly quick-release mounting assembly ball lock sleevebody 1417 is biased to a forward position by a pusher assemblyquick-release mounting assembly biasing device 1420. The pusher assemblyquick-release mounting assembly ball retainer 1418 is movably disposedwithin an associated pusher assembly housing mounting cavity 1404 andgenerally within an associated pusher assembly quick-release mountingassembly ball lock sleeve body. Each pusher assembly quick-releasemounting assembly ball retainer 1418 is biased to a forward position bya pusher assembly quick-release mounting assembly biasing device 1420.Further, each pusher assembly quick-release mounting assembly ball locksleeve body medial portion lug 1436 extends through an associated pusherassembly quick-release mounting assembly ball retainer lug slot 1450.Further, each pusher assembly quick-release mounting ball 1414 istrapped between an associated pusher assembly quick-release mountingassembly base 1412 and an associated pusher assembly quick-releasemounting assembly ball retainer 1418.

In this configuration, each quick-release mounting assembly 1410 isstructured to, and does, move between three configurations, an unengagedfirst configuration wherein no pusher pad is disposed within the pusherassembly quick-release mounting assembly base 1412, each of the pusherassembly quick-release mounting assembly ball lock sleeve body 1417 isbiased to a forward position relative to an associated pusher assemblyquick-release mounting assembly ball retainer 1418, and each of thepusher assembly quick-release mounting ball 1414 is biased toward aninner position, a release configuration wherein each of the pusherassembly quick-release mounting assembly ball lock sleeve body 1417 isbiased to a rearward position relative to an associated pusher assemblyquick-release mounting assembly ball retainer 1418, and each of thepusher assembly quick-release mounting ball 1414 is biased toward anouter position, and an engaged second configuration wherein a pusher pad1480 is disposed within the pusher assembly quick-release mountingassembly base 1412, each of the pusher assembly quick-release mountingassembly ball lock sleeve body 1417 is biased to a forward positionrelative to an associated pusher assembly quick-release mountingassembly ball retainer 1418, and each of the pusher assemblyquick-release mounting ball 1414 is biased toward an inner positionwherein each of the pusher assembly quick-release mounting ball 1414 isdisposed in an associated pusher pad body first end locking channel1488.

The pusher assembly pusher pads 1480 are substantially similar and onlyone is described. The pusher assembly pusher pad 1480 includes a toroidbody 1482 including a narrow first end 1484 and a wide second end 1486as well as defining a passage 1487. That is, the pusher assembly pusherpad body 1482 has a generally T-shaped cross-section. The pusherassembly pusher pad body first end 1484 includes a locking channel 1488on the outer surface thereof The pusher assembly pusher pad body 1482 iscoupled to the quick-release mounting assembly 1410 by inserting thepusher assembly pusher pad body first end 1484 into the pusher assemblyquick-release mounting assembly base 1412 until the pusher assemblypusher pad body first end 1484 displaces the quick-release mountingassembly number of balls 1414 outwardly. Further motion of the pusherassembly pusher pad body 1482 into the pusher assembly quick-releasemounting assembly base 1412 moves the pusher assembly pusher pad bodyfirst end locking channel 1488 into alignment with the quick-releasemounting assembly number of balls 1414. That is, the quick-releasemounting assembly number of balls 1414 are disposed in the pusherassembly pusher pad body first end locking channel 1488. This is thesecond configuration of the quick-release mounting assembly discussedabove.

The quick-release mounting assembly 1410 is structured to be, and is,actuated to move to the release configuration from the secondconfiguration by applying a bias to the pusher assembly quick-releasemounting assembly ball lock sleeve lug 1436 and moving it from a forwardposition to a rearward position within the pusher assembly housing bodycavity 1404. This actuation moves the pusher assembly quick-releasemounting assembly ball lock sleeve 1416 so that the pusher assemblyquick-release mounting assembly ball lock sleeve body first end taperedportion 1431 is disposed adjacent to the quick-release mounting assemblynumber of balls 1414 thereby allowing the quick-release mountingassembly number of balls 1414 to move radially outward. That is, thequick-release mounting assembly number of balls 1414 are no longerdisposed in the pusher assembly pusher pad body first end lockingchannel 1488. In this configuration, the pusher assembly pusher pad 1480is removable from the quick-release mounting assembly 1410. The pusherassembly quick-release mounting assembly ball lock sleeve lug 1436 is,in an exemplary embodiment, actuated by a generally cylindrical rod, orsimilar construct being inserted through the pusher assembly pusher padbody passage 1487. Thus, only an exceedingly limited number ofcouplings, i.e., one quick-release mounting assembly 1410, are used tocouple the pusher assembly body 1402 to the pusher assembly mountingassembly 1410.

Further, each pusher assembly pusher pad body second end 1486 includesan axially extending, arcuate lip 1490 structured to protect a can body1 as the can body 1 moves adjacent to a guide starwheel 1092. The pusherpad body second end lip 1490 includes a distal end 1492 that is, in anexemplary embodiment, tapered and/or resilient. Further, the pusher padbody second end lip 1490 extends over an arc of less than 180 degreesand, in an exemplary embodiment, about 140 degrees. The pusher pad bodysecond end lip 1490 is a can body 1 locator. As used herein, a “can bodylocator” is a construct structured to support a can body 1 and to alignthe can body 1 with a die assembly 1060 and to protect the can body 1 asthe can body 1 moves adjacent to a guide starwheel 1092.

As shown in FIG. 27, the forming station quick-change assembly 900further includes a quick-change die assembly 1500 (the elements thereofare also identified herein as part of the inboard turret assemblyprocess shaft assembly die assemblies 1060 and vice-versa).

As noted above, the process shaft assembly 1020 includes a plurality ofknockout ram mountings 1030, a plurality of knockout ram assemblies1040, a plurality of die assemblies 1060, and a die assembly support1080. That is, the die assembly support 1080 is, in an exemplaryembodiment, a torpid body 1082 that is structured to be, and is,coupled, directly coupled, or fixed to the process shaft assembly shaft1022. The die assembly support 1080 is further structured to support anumber of knockout ram mountings 1030, a plurality of knockout ramassemblies 1040, and a number of die assemblies 1060. As is known, aknockout ram mounting 1030 supports a knockout ram assembly 1040, and anassociated die assembly 1060. There are a plurality of sets of theseassociated elements which are generally similar. As such, the followingwill discuss one set of these associated elements. It is understood thatthe process shaft assembly 1020 includes a plurality of these associatedelements disposed about the process shaft assembly shaft 1022.

In an exemplary embodiment, the knockout ram mounting 1030 is a linearbearing 1032 disposed on the die assembly support 1080 and which extendsgenerally parallel to the axis of rotation of the process shaft assemblyshaft 1022. In this exemplary embodiment, the knockout ram mountinglinear bearing 1032 is a “substantially decoupled” linear bearing. Asused herein, a “substantially decoupled” linear bearing means a linearbearing that is coupled to a number of forming constructs such as, butnot limited to a die, wherein a rotational coupling is disposed betweenall forming constructs and the linear bearing so that only force in asingle direction is applied to the linear bearing.

The knockout ram assembly 1040 includes a body 1041 that is an inner diemounting 1042. That is, the knockout ram assembly inner die mounting1042 supports the inner die 1560 and is structured to, and does,reciprocate over the knockout ram mounting 1030. Generally, the knockoutram assembly inner die mounting 1042 defines a bearing channel thatcorresponds to the knockout ram mounting linear bearing 1032. Theknockout ram assembly inner die mounting 1042 further includes two camfollowers 1044, 1046 that operatively engage the inboard turret assemblycam ring 1010. In one embodiment, the knockout ram assembly inner diemounting 1042 defines a cavity 1047 that is open on one end. In anotherembodiment, the knockout ram assembly inner die mounting 1042 includes arotational coupling lug 1048 located on a first end (which includes theforward surface of the inner die mounting 1042) of the knockout ramassembly inner die mounting 1042. As used herein, a “rotational couplinglug” is a toroid lug having an L-shaped cross-section.

There are, generally, two embodiments of the quick-change die assembly1500 although elements of each embodiment are, in another embodiment,combined. In both embodiments, the quick-change die assembly 1500includes an outer die mounting 1502, an outer die 1504, an outer diequick-release coupling 1506, an inner die mounting 1512, an inner dieassembly 1514, and an inner die quick-release coupling 1516. As usedherein, an “outer die quick-release coupling” and/or an “inner diequick-release coupling” means a coupling wherein the die coupled to amounting via the “quick-release coupling” is structured to be releasedfollowing the actuation of one of a limited number of couplings, asignificantly limited number of couplings, a very limited number ofcouplings, or an exceedingly limited number of couplings, and, whereinthe couplings are a retained coupling, a release coupling, a retainedrelease coupling, or a reduced actuation coupling. As shown in FIGS.35A-39, the outer die 1504 is coupled, directly coupled, or fixed to theouter die mounting 1502 by the outer die quick-release coupling 1506.The inner die assembly 1514 is coupled, directly coupled, or fixed tothe inner die mounting 1512 by the inner die quick-release coupling1516.

The outer die 1504 includes a generally toroid body 1520 having a shapedinner surface. As is known, the outer die shaped inner surface isstructured to, and does, reduce the diameter of a can body first end 6and generally includes a first radius portion and a second radiusportion. The outer die body 1520 includes a proximal, first end 1522(disposed further from the gap 1001 when installed), a medial portion1523 and a distal, second end 1524 (disposed closer from the gap 1001when installed). In one exemplary embodiment, the outer die body firstend 1522 includes an outwardly radially extending annular locking lip1525 that extends about the outer die body first end 1522.

In another embodiment, the outer die body first end 1522 includes anumber of outwardly radially extending, arced locking members 1540. Asused herein, an “arced locking member” is an extension that extends overan arc that is less than about 60° and which is structured to engagewith opposed arced locking members. In the embodiment shown, there arethree arced locking members 1540 extending about 60° each.

As shown in FIGS. 40-43, the inner die assembly 1514 includes an innerdie 1560 and an inner die support 1562. The inner die 1560 includes atoroid body 1564 with an inwardly extending flange (not numbered). Theinner die body 1564 flange defines a passage. The inner die support 1562includes a body 1565 having a first end 1566 and a second end 1568. Theinner die support body first end 1566 defines a coupling 1569, such as,but not limited to, a threaded bore, to which the inner die body 1564 iscoupled. For example, a fastener (not numbered) extends through theinner die body 1564 flange and into the inner die support body first endcoupling 1569, i.e., the threaded bore. In one embodiment, the inner diesupport body 1565 is generally toroid and the inner die support bodysecond end 1568 includes an annular locking channel 1570 on the outersurface. In another embodiment, not shown, the inner die body isgenerally a parallelepiped and the inner die support body second end1568 includes a radial access cavity 1572. As used herein, a “radialaccess cavity” means a cavity that is structured to be, and is, coupledto a rotational coupling lug and which is structured to, and does,engage the rotational coupling lug while moving generally radiallyrelative to a process shaft assembly shaft 1022.

In one embodiment, shown in FIG. 371, the outer die quick-releasecoupling 1506 includes a generally toroid body 1580 with a number ofbayonet pin channels 1582, a bayonet pin channel cutout 1584, and aninwardly, radially extending locking lip 1586. The outer diequick-release coupling body bayonet pin channels 1582 are generallysimilar and only one is described. Each outer die quick-release couplingbody bayonet pin channel 1582 is an elongated obround channel that isdisposed at an angle relative to the axis of rotation of the processshaft assembly shaft 1022 (when installed). Further, the outer diequick-release coupling body bayonet pin channels 1582 are defined by acompliant material and include offset ends. As used herein, an “offsetend” is an end that is shifted to one lateral side relative to alongitudinal axis of the channel.

Further, a bayonet pin channel cutout 1584, as used herein, means a thinportion of the outer die quick-release coupling body 1580 that isstructured to not engage, or otherwise contact, a bayonet pin. That is,in a toroid body, the bayonet pin channel is a thinned portion whereinthe bayonet pins fit under the bayonet pin channel cutout 1584.

In this embodiment, shown in FIG. 37A, the outer die mounting 1502includes a generally planar body 1590 with a passage 1592 therethroughand a collar 1594 disposed about the outer die mounting body passage1592. The outer die mounting body 1590 is, in one embodiment, agenerally toroid disk 1596 that is, coupled, directly coupled, or fixedto the process shaft assembly shaft 1022 and which includes a pluralityof passages 1592, i.e., one for each die assembly 1060. in thisembodiment, outer die mounting body 1590 includes a number of radiallyextending bayonet pins 1600, i.e., rigid pins. In an exemplaryembodiment, there are a plurality of outer die body bayonet pins 1600disposed generally evenly about the outer die body 1600 (three shown atabout 120° apart).

In this embodiment, the outer die quick-release coupling 1506 operatesas follows. The outer die 1504 is disposed on the front surface of theouter die mounting collar 1594. The outer die quick-release couplingbody 1580 is moved over the outer die 1504 with the outer die mountingcollar bayonet pins 1600 passing under the bayonet pin channel cutout1584 into the outer die quick-release coupling body bayonet pin channels1582. In this configuration, the outer die quick-release coupling bodyinwardly, radially extending locking lip 1586 engages the outer die bodyfirst end locking, lip 1525. When the outer die quick-release couplingbody 1580 is rotated, and because the outer die quick-release couplingbody bayonet pin channel 1582 is disposed at an angle as describedabove, the outer die quick-release coupling body 1580 is drawn towardthe outer die mounting collar 1594. This, in turn, biases the outer die1504 against the outer die mounting collar 1594. Further, in anotherembodiment, a compliant ring 1602 is disposed between the outer diequick-release coupling body 1580 and the outer die 1504.

In another embodiment, FIGS. 35A-35E the outer die quick-releasecoupling 1506 includes a toroid body with a number of inwardly radiallyextending, arced locking members 1542. The outer die quick-releasecoupling body is coupled, directly coupled, or fixed to the outer diemounting collar or a support element fixed to the process shaft assemblyshaft 1022. That is, for example, the outer die quick-release coupling1506 includes a threaded end and a support disk (which is fixed to theprocess shaft assembly shaft 1022) including a threaded borecorresponding to the outer die quick-release coupling body 1580 threadedend. The outer die quick-release coupling 1506 is fixed to the supportdisk. The outer die quick-release coupling 1506 includes a number ofinwardly radially extending, arced locking members. The outer die body1520 is disposed within the outer die quick-release coupling 1506, i.e.,between the outer die quick-release coupling body 1580 and the collar1594 or support disk, and is structured to move between an unlockedfirst position, wherein the outer die body locking members 1540 are notaligned with the outer die quick-release coupling body locking members1542 (and, therefore, can be moved past the outer die quick-releasecoupling, body locking members 1542 when moved away from the collar orsupport disk), and, a locked second position, wherein the outer die bodylocking members 1540 are aligned with the outer die quick-releasecoupling body locking members 1542. Further, the outer die quick-releasecoupling body locking members 1542 and/or the outer die body lockingmembers 1540 are made from a compliant material, or, have a sufficientthickness, so that when the elements are in the locked second positionthe outer die body is biased against the collar or the support disk.

In this embodiment, the inner die support body second end 1568 includesthe annular locking channel 1570, as described above. The inner dieassembly 1514 is coupled to the knockout ram assembly inner die mountingcavity 1047 (also identified herein as the “knockout ram assembly bodycavity” 1047) by a quick-release mounting assembly 1410 that issubstantially similar to the one described above. That is, thequick-release mounting assembly 1410 is disposed in the knockout ramassembly body cavity 1047 (which is threaded or otherwise structured tobe coupled, directly coupled, or fixed to the quick-release mountingassembly 1410). The inner die support body second end locking channel1570 engages the ball(s) of the quick-release mounting assembly 1410.

In another embodiment, the outer die mounting, the outer die, the outerdie quick-release coupling, the inner die mounting, the inner dieassembly, and the inner die quick-release coupling, are a unit assembly.In this embodiment, shown in FIGS. 44-45, the process shaft assemblyshaft 1022 includes a mounting disk 1700. The process shaft assemblyshaft mounting disk 1700 includes a body 1702 with a number ofperipheral, radial cutouts 1704. The mounting disk body radial cutouts1704 include axially extending locking channels 1706. As shown, themounting <disk body radial cutouts 1704 are generally U-shaped and opentoward the radial surface of the process shaft assembly shaft mountingdisk body 1702.

In this embodiment, the outer die mounting includes a generally planarbody that is structured to correspond to the mounting disk body radialcutouts. The outer die mounting body includes a radial surface (which isthe surface generally parallel to the mounting disk body 1702 radialsurface). The outer die quick-release coupling includes a locking pawlassembly 1750 disposed on the outer die mounting body radial surface.The locking pawl assembly includes a pivot pin 1751 and an elongatedpawl body 1752. The locking pawl assembly pawl body 1752 includes afirst end 1754, a medial portion 1756, and a second end 1758. Thelocking pawl assembly pawl body medial portion defines a pivot pinpassage 1760. The locking pawl assembly pawl body first end 1754 and thelocking pawl assembly pawl body second end 1758 are structured to engagethe mounting disk body locking channels 1706. The locking pawl assemblypawl body 1752 is rotatably coupled to the locking pawl assembly pivotpin 1751. In this configuration, the locking pawl assembly 1750 isstructured to move between an unlocked, first configuration, wherein thelocking pawl assembly pawl body first end 1754 and the locking pawlassembly pawl body second end 1758 do not engage the mounting disk bodylocking channels 1706, and, a locked, second configuration wherein thelocking pawl assembly pawl body first end 1754 and the locking pawlassembly pawl body second end engage 1758 the mounting disk body lockingchannels 1706.

Further, in this embodiment, the inner die support body second end 1568includes a radial access cavity 1572 and the inner die mounting 1042includes a rotational coupling lug 1048. Thus, in this configuration,the outer die and the inner die, and the elements coupled thereto, arestructured to be, and are, removed from the process shaft assembly shaft1022 as a unit assembly. Further, these elements, i.e., the unitassembly, are moved radially relative to the process shaft assemblyshaft 1022.

As is known, it is desirable to apply positive pressure to the interiorof the can bodies 1 as the can bodies 1 are being formed at the formingstations 20. The positive pressure helps the can bodies resist damageduring forming. Accordingly, each inboard turret assembly 1000, or eachprocess shaft assembly 1020 includes a rotary manifold assembly 1800structured to supply positive pressure to each process shaft assemblydie assembly 1060. It is understood that the process shaft assemblyshaft 1022, or elements fixed thereto, define a number of generallylongitudinal passages 1028 each having an inlet 1027 and an outlet 1029.Each process shaft assembly shaft outlet 1029 is structured to be, andis, in fluid communication with an associated process shaft assembly dieassembly 1060. Each process shaft assembly shaft inlet 1027 is disposedadjacent, or immediately adjacent, the rotary manifold assembly 1800.

In an exemplary embodiment, as shown in FIGS. 46-48, the rotary manifoldassembly 1800 includes an outer body assembly 1810 and an inner body1900. As discussed herein, the various seals, bearings, etc., areidentified as part of the manifold assembly outer body assembly 1810.That is, the manifold assembly outer body assembly 1810 includes agenerally toxoid outer body 1812, a number of bearing assemblies 1820, anumber of seals 1840, and a number of fluid couplings 1860. The manifoldassembly outer body 1812 is structured to be, and is, coupled in agenerally fixed position to the frame assembly 12. As used herein, a“generally fixed position” means that one element is able to rotateabout, but not with, a generally circular or cylindrical element but notmove longitudinally on that element. Thus, the manifold assembly outerbody 1812 is structured to rotate about, but not with, the process shaftassembly shaft 1022, as discussed below.

The manifold assembly outer body assembly body 1812 defines a number ofradial passages 1814. Each manifold assembly outer body assembly bodyradial passage 1814 includes an inlet 1816 and an outlet 1818. Themanifold assembly outer body assembly body radial passages 1814 aredisposed in a common axial plane within the manifold assembly outer bodyassembly body 1812. In an exemplary embodiment, the plane of themanifold assembly outer body assembly body radial passages 1814 isdisposed substantially at the middle of the manifold assembly outer bodyassembly body 1812.

Further, the manifold assembly outer body assembly body 1812 includes aninner surface 1813. The manifold assembly outer body assembly body innersurface 1813 includes a number of “scallops” 1815. As used herein, a“scallop” means a generally concave cavity. Each manifold assembly outerbody assembly body inner surface scallop 1815 includes an axialcenterline 1817 (a centerline when viewed axially). Each manifoldassembly outer body assembly body inner surface scallop 1815 is disposedabout (encircling) a manifold assembly outer body assembly body radialpassage outlet 1818. As shown, however, the manifold assembly outer bodyassembly body radial passage outlet 1818 is not, in an exemplaryembodiment, disposed on the manifold assembly outer body assembly bodyinner surface scallop axial centerline 1817. That is, each of themanifold assembly outer body assembly body radial passage outlet 1818 isoffset relative to the manifold assembly outer body assembly body innersurface scallop axial centerline 1817.

Each manifold assembly outer body assembly fluid coupling 1860 isstructured to be, and is, in fluid communication with a pressureassembly (not shown) structured to produce positive or negativepressure. As discussed herein, the pressure assembly is structured toproduce positive pressure. Further, each manifold assembly outer bodyassembly fluid coupling 1860 is structured to be, and is, in fluidcommunication with an associated manifold assembly outer body assemblybody radial passage inlet 1816.

The generally toroid manifold assembly inner body 1900 defines a numberof right angle passages 1902. As used herein, a right angle passage on atoroid body extends from a radial surface on the toroid body to an axialsurface on the toroid body. Each manifold assembly inner body passage1902 includes an inlet 1904 and an outlet 1906. The manifold assemblyinner body 1900 is rotatably disposed within the manifold assembly outerbody assembly body 1812.

Each manifold assembly outer body assembly bearing assembly 1820 isdisposed between the manifold assembly outer body assembly body 1812 andthe inner body 1900. In an exemplary embodiment, there are threemanifold assembly outer body assembly bearing assemblies; a firstannular manifold assembly outer body assembly bearing assembly 1822, asecond annular manifold assembly outer body assembly bearing assembly1824, and an annular manifold assembly outer body assembly low frictionbearing 1826. As used herein, an “annular” bearing or seal is abearing/seal that extends circumferentially about a generallycylindrical body. In an exemplary embodiment, the first annular manifoldassembly outer body assembly bearing assembly 1822 and the secondannular manifold assembly outer body assembly bearing assembly 1824 are“sealed” bearings. As used herein, a “sealed” bearing includes tworaces, or similar constructs, that are sealingly coupled to each otherand which include bearing elements such as, but not limited to, ballbearings, disposed between the races. In an exemplary embodiment, theannular manifold assembly outer body assembly low friction bearing 1826is an annular bearing including a number of radial passages 1828. Eachannular manifold assembly outer body assembly low friction bearingpassage 1828 is structured to correspond to (be aligned with) a manifoldassembly outer body assembly body radial passage outlet 1818.

The first annular manifold assembly outer body assembly bearing assembly1822 is disposed on a first axial side of the manifold assembly outerbody assembly body radial passages 1814. The second annular manifoldassembly outer body assembly bearing assembly 1824 is disposed on asecond axial side of the manifold assembly outer body assembly bodyradial passages 1814. The annular manifold assembly outer body assemblylow friction bearing 1826 is disposed in the plane of the manifoldassembly outer body assembly body radial passages 1814 with each annularmanifold assembly outer body assembly low friction bearing passage 1828aligned with an associated manifold assembly outer body assembly bodyradial passage 1814.

In an exemplary embodiment, the manifold assembly outer body assemblynumber of seals 1840 includes a first annular seal 1842 and a secondannular seal 1844. The first seal 1842 is disposed between the firstmanifold assembly outer body assembly bearing assembly 1822 and themanifold assembly outer body assembly body radial passages 1814 Thesecond seal 1844 is disposed between the second manifold assembly outerbody assembly bearing assembly 1824 and the manifold assembly outer bodyassembly body radial passages 1814. That is, the manifold assembly outerbody assembly number of seals 1840 are structured to, and do, resistpositive pressure fluid from impinging upon the first annular manifoldassembly outer body assembly bearing assembly 1822 and the secondannular manifold assembly outer body assembly bearing assembly 1824.

The rotary manifold assembly 1800 is assembled as follows. The manifoldassembly inner body 1900 is rotatably disposed within the manifoldassembly outer body assembly body 1812 with the number of bearingassemblies 1820 and the number of seals 1840 disposed therebetween asdescribed above. The manifold assembly inner body 1900 is fixed to theprocess shaft assembly body 1022. Thus, the manifold assembly inner body1900 rotates with the process shaft assembly body 1022. Each manifoldassembly outer body assembly fluid coupling 1860 is coupled to, andplaced in fluid communication with, an associated manifold assemblyouter body assembly body radial passage inlet 1816. The manifoldassembly outer body assembly body 1812 is coupled in a generally fixedposition to the frame assembly 12. That is, the manifold assembly outerbody assembly body 1812 is circumferentially rotatable relative to theaxis of rotation of the process shaft assembly body 1022. Thus, themanifold assembly outer body assembly body 1812 can be rotated about theprocess shaft assembly body 1022.

In this configuration, each manifold assembly inner body passage inlet1904 is structured to be, and is, discontinuously in fluid communicationwith the manifold assembly outer body assembly body passage outlets1818. That is, when a manifold assembly inner body passage inlet 1904rotates to be aligned with a manifold assembly outer body assembly bodypassage outlets 1818 (or an associated scallop 1815), the manifoldassembly inner body passage, inlet 1904 is in fluid communication withthat manifold assembly outer body assembly body passage outlet 1818. Asthe manifold assembly inner body passage inlet 1904 continues to rotate,the manifold assembly inner body passage inlet 1904 moves out of fluidcommunication with that manifold assembly outer body assembly bodypassage outlet 1818. Further rotation of the manifold assembly innerbody passage inlet 1904 moves the rotation of the manifold assemblyinner body passage inlet 1904 into fluid communication with the nextmanifold assembly outer body assembly body passage outlet 1818. As usedherein, this type of intermittent fluid communication, is defined as“discontinuously in fluid communication.” Similarly, each manifoldassembly inner body passage outlet 1906 is structured to be, and is,discontinuously in fluid communication with the process shaft assemblybody passages inlets 1027.

Further, in this configuration, the interface between the manifoldassembly outer body assembly 1810 and the manifold assembly inner body1900 is an axially extending interface. This solves the problems notedabove. Further, in this configuration, neither the manifold assemblyouter body assembly 1810 nor the manifold assembly inner body 1900includes a seal biasing assembly. Thus, no seal is biased toward therotating elements, i.e., the manifold assembly inner body 1900. Thissolves the problems noted above.

The drive assembly 2000 is structured to, and does, provide rotationalmotion to au element of each processing station 20. That is, as shown inFIGS. 49 and 50, each processing station 20 includes a number of driveshafts 2002 such as, but not limited to, the rotating shaft assemblyrotating shaft 416. As used herein, any of the “number of drive shafts2002” represents a drive shaft which is a part of a processing station20; selected drive shafts 2002 have been discussed above and have anadditional reference number associated therewith. In an exemplaryembodiment, and at a processing station 20, the drive assembly 2000 isoperatively coupled to the rotating shaft assembly rotating shaft 416and the process shaft assembly shaft 1022.

As shown, each processing station 20 includes a processing station firstdrive shaft 2002A and a processing station second drive shaft 2002B.Further, the number of processing stations 20 includes a number ofstation pairs 2004. As used herein, a “station pair” means two adjacentprocessing stations; a first station 2004A and a second station 2004B.As shown, the necker machine 10 includes a plurality of station pairs2004. For example, as shown, there is a first station pair 2004′ (whichincludes a first station 2004A′ and a second station 2004B′), and, asecond station pair 2004″ (which includes a first station 2004A″ and asecond station 2004B″).

In an exemplary embodiment, the drive assembly 2000 includes a pluralityof motors 2010, a plurality of drive wheel assemblies 2020, and a numberof timing/drive belts 2080. Each drive assembly motor 2010 includes anoutput shaft 2012 and a drive wheel 2014. As used herein, a “drivewheel” is a wheel that is structured to, and does, operatively engagetiming/drive belts 2080. That is, in an exemplary embodiment, each“drive wheel” includes teeth that correspond to teeth on a timing/drivebelt 2080. Further, as used herein, a “drive wheel” is fixed to aprocessing station drive shaft 2002 or a motor output shaft 2012.Further, each drive assembly motor 2010 includes an angular contactbearing 2016. As used herein, an “angular contact bearing” is a bearingthat is structured to, and does, decouple the axial loads applied to theangular contact bearing from the shaft about which the angular contactbearing 2016 is disposed. The drive assembly motor angular contactbearing 2016 is disposed about the drive assembly motor output shaft2012. Thus, each drive assembly motor output shaft 2012 is decoupledfrom all axial loads.

Each drive wheel assembly 2020 is structured to be, and is, operativelycoupled to an associated processing station drive shaft 2002. Each drivewheel assembly 2020 includes a driver assembly 2030 and a drivenassembly 2040. Each drive wheel assembly driver assembly 2030 includes afirst drive wheel 2032 and a second drive wheel 2034, and, each drivewheel assembly driven assembly 2040 includes a first drive wheel 2042and a second >drive wheel 2044. Each drive wheel assembly driverassembly 2030 is directly and operatively coupled to a motor outputshaft 2012. As used herein, “directly and operatively coupled” meansthat a timing/drive belt 2080 extends directly between the two elementsthat are “directly and operatively coupled.” Each drive wheel assemblydriven assembly 2040 is not “directly and operatively coupled” to amotor output shaft 2012.

That is, each drive wheel assembly driver assembly 2030, i.e., the drivefirst wheel 2032 and a second drive wheel 2034 thereof, is operativelycoupled to the drive shafts 2002 of a first station 2004A and each drivewheel assembly driven assembly 2040, i.e., the first drive wheel 2042and the second drive wheel 2044 thereof, is operatively coupled to thedrive shafts 2002 of a second station 2004B. Further, to form the meshedlink among the number of motors, at least one timing/drive belts 2080extends between, and is operatively coupled to, adjacent station pairs2004. That is, for example a timing/drive belt 2080 from one drive wheelassembly 2020 extends between, and is operatively coupled to an adjacentwheel assembly 2020. This is accomplished by including one double widedrive wheel in each drive wheel assembly 2020. As used herein, a “doublewide drive wheel” is a drive wheel having an axial length sufficient toaccommodate, a plurality of timing/drive belts 2080. As shown, eachdrive wheel assembly driver assembly first drive wheel 2032 is a doublewide drive wheel. Thus, at least one timing/drive belt 2080 isoperatively coupled to both a first station pair 2004′ and a secondstation pair 2004″.

Further, each drive wheel 2014, 2032, 2034, 2042, 2044 is a“cantilevered drive wheel.” As used herein, a “cantilevered drive wheel”means a drive wheel wherein the drive wheel is outboard of any supportbearings; this enables the timing/drive belts 2080 to be changed withoutremoving any parts from the necker machine 10. Further, all the drivewheels 2014, 2032, 2034, 2042, 2044 are disposed generally in the sameplane. Thus, the drive elements, i.e., the timing/drive belts 2080 arein easy to access locations. As used herein, an “easy to access”location is one that requires the removal of one or more othercomponents prior to accessing the fastener wherein the “other component”is an access device such as, but not limited to, a door or housingpanel.

In an exemplary embodiment, each drive wheel assembly 2020 includes anumber of tensioner assemblies 2050. As shown, each drive wheel assemblydriver assembly 2030 and each drive wheel assembly driven assembly 2040includes a tensioner assembly 2050. The tensioner assemblies 2050 aresubstantially similar and only one is described. The tensioner assembly2050 includes a tensioner assembly mounting 2052, a tensioner wheel 2054and a tensioner device 2056. Each tensioner assembly mounting 2052includes a hub 2060 with a first radial arm 2062 and a second radial arm2064, and, a bracket 2066. The tensioner assembly mounting hub 2060 is,in an exemplary embodiment, a toroid body that is disposed about aprocess station drive shaft 2002. The tensioner assembly tensioner wheel2054 (which is similar to a drive wheel but is not fixed to a driveshaft 2002) is rotatably coupled to the tensioner assembly mounting hubfirst radial arm 2062. It is understood that a timing/drive belt 2080operatively engages the tensioner assembly tensioner wheel 2054.

The tensioner assembly tensioner device 2056 is structured to detect thetension in an associated timing/drive belt 2080, i.e., the timing/drivebelt 2080 operatively engaging the drive wheel 2014, 2032, 2034, 2042,2044 to which the tensioner assembly 2050 is directly coupled. Eachtensioner assembly tensioner device 2056 includes a sensor 2070, a firstinput member 2072 and a second input member 2074. In an exemplaryembodiment, the tensioner assembly tensioner device sensor 2070 is aload cell. Both the tensioner assembly tensioner device first inputmember 2072 and the tensioner assembly tensioner device second inputmember 2074 are operatively coupled to the tensioner assembly tensionerdevice sensor 2070. The tensioner assembly tensioner device first inputmember 2072 is operatively coupled to the tensioner assembly mountinghub second radial arm 2064. The tensioner assembly tensioner devicesecond input member 2074 is operatively coupled to the tensionerassembly mounting bracket 2066. The tensioner assembly mounting bracket2066 is fixed to the frame assembly 12. Further, the tensioner assemblytensioner device 2056 is disposed generally in the same plane as thedrive wheels 2014, 2032, 2034, 2042, 2044. In an exemplary embodiment,the tensioner assembly tensioner device 2056 is structured to adjust thetension in an associated timing/drive belt 2080.

Each timing drive belt 2080 is structured to be, and is, operativelycoupled to each drive wheel assembly, i.e., all the timing/drive belts2080 are operatively coupled to all the drive wheel assemblies 2020. Asused herein, a “timing/drive belt” is a belt that is structured to, anddoes, provide a drive function and a timing function. In an exemplaryembodiment, each timing/drive belts 2080 includes an elongated body 2082having a first side 2084 and a second side 2086. Both timing/drive beltbody first side and second side 2084, 2086, have teeth thereon. In anexemplary embodiment, all the timing/drive belts 2080 are operativelycoupled to all the drive wheel assembly drive wheels 2032, 2034, 2042,2044. In this configuration, the timing/drive belts 2080 form a meshedlink among the plurality of motors 2010. As used herein, a “meshed link”means a configuration wherein all the tinting/chive belts 2080 areoperatively coupled to all the drive wheel assemblies 2020. Further, adrive assembly 2000 utilizing timing/drive belts 2080 does not require alubrication system for a drive shaft linkage. A drive assembly 2000 inthe configuration describe herein solves the problems noted above.

While specific embodiments of the invention have been described indetail, it will be appreciated by those skilled in the art that variousmodifications and alternatives to those details could be developed inlight of the overall teachings of the disclosure. Accordingly, theparticular arrangements disclosed are meant to be illustrative only andnot limiting as to the scope of invention which is to be given the fullbreadth of the claims appended and any and all equivalents thereof.

What is claimed is:
 1. An infeed assembly for a necker machine, saidnecker machine including a frame assembly, said necker machine frameassembly having an upstream end and a downstream end, said neckermachine defining a work path having an upstream end and a downstreamend, said infeed assembly comprising: a full inspection assembly; andsaid full inspection assembly structured to be coupled to said neckermachine frame assembly.
 2. The infeed assembly of claim 1 wherein saidfull inspection assembly is an upstream inspection assembly,
 3. Theinfeed assembly of claim 1 wherein: said full inspection assemblyincludes a number of inspection devices; said full inspection assemblyincludes a mounting assembly; and said full inspection assembly mountingassembly structured to couple each inspection device to said neckermachine frame assembly,
 4. The infeed assembly of claim 3 wherein: saidmounting assembly includes a number of mounting assembly guides; andeach mounting assembly guide disposed adjacent an inspection device. 5.The infeed assembly of claim 4 wherein: said full inspection assemblyincludes a first vacuum starwheel and a second vacuum starwheel; andsaid full inspection assembly first vacuum starwheel disposed aneffective distance from said full inspection assembly second vacuumstarwheel.
 6. The infeed assembly of claim 4 wherein: said number ofinspection devices includes a sidewall damage inspection assembly and acut edge damage inspection assembly; said sidewall damage inspectionassembly includes a camera; said cut edge damage inspection assemblyincludes a camera; said mounting assembly includes a dual-camera mount;said dual-camera mount disposed adjacent said work path; and saiddual-camera mount structured to position said sidewall damage inspectionassembly camera to focus on a can body sidewall, and, position said cutedge damage inspection assembly camera to focus on a can body first end.7. The infeed assembly of claim 6 wherein said cut edge damageinspection assembly camera is coupled to said dual-camera mount withsufficient spacing between said cut edge damage inspection assemblycamera and said work path to provide a cut edge damage inspectionassembly camera focal length.
 8. The infeed assembly of claim 6 wherein:said sidewall damage inspection assembly camera is a dual-purposecamera; and said cut edge damage inspection assembly camera is adual-purpose camera.
 9. The infeed assembly of claim 4 wherein: saidnumber of inspection devices includes a label verification assembly andan un-printed can inspection assembly; said mounting assembly includinga 360° mounting; said label verification assembly coupled to saidmounting assembly 360° mounting; and said un-printed can inspectionassembly coupled to said mounting assembly 360° mounting.
 10. The infeedassembly of claim 9 wherein: said mounting, assembly 360° mounting isdisposed adjacent said work path; said label verification assemblystructured to inspect a can body as the can body moves along the workpath; and said un-printed can inspection assembly structured to inspect360° about a can body as the can body moves along the work path.
 11. Theinfeed assembly of claim 3 wherein: said full inspection assemblyincludes an ejection assembly; and said full inspection assemblyejection assembly structured to eject a deficient can body from saidwork path.
 12. The infeed assembly of claim 11 wherein said fullinspection assembly ejection assembly is an upstream ejection assembly.13. The infeed assembly of claim 12 wherein: said mounting assemblyincludes a number of mounting assembly guides; and each mountingassembly guide disposed adjacent an inspection device.
 14. A neckermachine comprising: a frame assembly having an upstream end and adownstream end; an infeed assembly including a full inspection assembly;and said full inspection assembly coupled to said necker machine frameassembly upstream end.
 15. The necker machine of claim 14 wherein saidfull inspection assembly is an upstream inspection assembly.
 16. Thenecker machine of claim 14 wherein: said full inspection assemblyincludes a number of inspection devices; said full inspection assemblyincludes a mounting assembly; and said full inspection assembly mountingassembly structured to couple each inspection device to said neckermachine frame assembly.
 17. The necker machine of claim 16 wherein: saidmounting assembly includes a number of mounting assembly guides; andeach mounting assembly guide disposed adjacent an inspection device. 18.The necker machine of claim 17 wherein: said full inspection assemblyincludes a first vacuum starwheel and a second vacuum starwheel; andsaid full inspection assembly first vacuum starwheel disposed aneffective distance from said full inspection assembly vacuum secondstarwheel.
 19. The necker machine of claim 17 wherein: said number ofinspection devices includes a sidewall damage inspection assembly and acut edge damage inspection assembly; said sidewall damage inspectionassembly includes a camera; said cut edge damage inspection assemblyincludes a camera; said mounting assembly includes a dual-camera mount;said dual-camera mount disposed adjacent said work path; and saiddual-camera mount structured to position said sidewall damage inspectionassembly camera to focus on a can body sidewall, and, position said cutedge damage inspection assembly camera to focus on a can body first end.20. The necker machine of claim 19 wherein said cut edge damageinspection assembly camera is coupled to said dual-camera mount withsufficient spacing between said cut edge damage inspection assemblycamera and said work path to provide a cut edge damage, inspectionassembly camera focal length.